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1 POLITECNICO DI MILANO Department of Civil and Environmental Engineering PhD course in Environmental and Infrastructure Engineering EDDY COVARIANCE MEASUREMENTS IN THE PO VALLEY: REPRESENTATIVENESS AND ACCURACY Chair of the doctoral program: Prof. Fernando Sansò Tutor: Doctoral dissertation of: Daniele Masseroni Matr. 753709 Year 2013 Cicle XXV

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Page 1: EDDY COVARIANCE MEASUREMENTS IN THE PO VALLEY ... · EDDY COVARIANCE MEASUREMENTS IN THE PO VALLEY: REPRESENTATIVENESS AND ACCURACY Chair of the doctoral program: Prof. Fernando Sansò

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POLITECNICO DI MILANO

Department of Civil and Environmental Engineering

PhD course in Environmental and Infrastructure Engineering

EDDY COVARIANCE MEASUREMENTS IN THE PO

VALLEY: REPRESENTATIVENESS AND ACCURACY

Chair of the doctoral program:

Prof. Fernando Sansò

Tutor:

Doctoral dissertation of:

Daniele Masseroni

Matr. 753709

Year 2013 – Cicle XXV

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Index

General Abstract ........................................................................................................... 6

General Introduction .................................................................................................... 8

Eddy covariance technique ....................................................................................... 8

References .............................................................................................................. 10

(Chapter 1) - Impact of data corrections on turbulent flux measurements ........ 11

Abstract .................................................................................................................. 11

Introduction ............................................................................................................ 11

Data collection ........................................................................................................ 13

Preliminary processes for correction procedure ..................................................... 13

Axis rotation for tilt correction ............................................................................... 13

Double rotation method .......................................................................................... 14

Spike removal ......................................................................................................... 14

Time lag compensation .......................................................................................... 14

Covariance maximization method .......................................................................... 15

Detrending .............................................................................................................. 15

Linear detrending ................................................................................................... 15

Calculating fluxes ................................................................................................... 16

Uncorrected fluxes – level 0 ................................................................................... 16

Spectral correction factors – level 1 ....................................................................... 17

Corrected fluxes – level 2 and 3 ............................................................................. 19

Results .................................................................................................................... 20

Effect of the preliminary processes on raw data .................................................... 20

Effect of the preliminary processes on uncorrected fluxes .................................... 22

Effect of the spectral corrections on turbulent fluxes ............................................ 24

Flux loss in function of air temperature and relative humidity .............................. 25

Flux loss in function of wind velocity and friction velocity .................................. 27

Flux loss in function of stability parameter ............................................................ 27

Daily and seasonal trend of flux losses .................................................................. 28

Effect of the WPL and VD corrections on fluxes at level 3 ................................... 29

Quality of fluxes ..................................................................................................... 31

Energy balance closure ........................................................................................... 34

Fluxes directly obtained from 30 minutes averaged data ....................................... 35

PEC software features ............................................................................................ 36

PEC fluxes in comparison with Eddy Pro 4.0 fluxes ............................................. 36

Energy balance closure with PEC fluxes ............................................................... 38

Conclusion .............................................................................................................. 38

References .............................................................................................................. 39

(Chapter 2) – Energy balance closure of an eddy covariance station: limitations and

improvements ........................................................................................................... 43

Abstract .................................................................................................................. 43

Introduction ............................................................................................................ 43

Instruments, data collection and site description ................................................... 45

The energy balance closure problem ...................................................................... 46

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Effect of data corrections ....................................................................................... 47

Effect of storage terms ........................................................................................... 48

Effect of time aggregation ...................................................................................... 51

Effect of scale differences in fluxes measurement ................................................. 52

Effect of turbulent mixing ...................................................................................... 54

Effect of vegetation ................................................................................................ 56

Effect of seasonality ............................................................................................... 57

Random error ......................................................................................................... 59

Conclusion ............................................................................................................. 60

References .............................................................................................................. 61

(Chapter 3) – Experimental data about the spatial variability of scalar fluxes across maize

field in Po Valley and comparison with theoretical footprint model predictions66

Abstract .................................................................................................................. 66

Introduction ............................................................................................................ 66

What is the importance of this experiment? ........................................................... 69

Theoretical background .......................................................................................... 69

Hsieh Model ........................................................................................................... 70

Kormann Model ..................................................................................................... 71

Study site, instruments and data ............................................................................. 71

Site characteristics.................................................................................................. 71

Instruments ............................................................................................................. 72

Data corrections ..................................................................................................... 72

Fixed eddy covariance stations (A1 and A2) ......................................................... 73

Experimental execution .......................................................................................... 74

Results .................................................................................................................... 76

Flux measurements across the fields ...................................................................... 76

Experimental data compared with footprint model predictions ............................. 78

Discussions............................................................................................................. 80

Conclusion ............................................................................................................. 81

References .............................................................................................................. 81

General Conclusion .................................................................................................... 85

Acknowledges ............................................................................................................ 86

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General Abstract

This PhD work is mainly focused on researching utilities for increasing the micrometeorological

flux reliabilities. Micrometeorological stations, which use the eddy covariance technique to

estimate turbulent fluxes in the surface layer, are generally located in different agricultural fields

to assess evapotranspiration and carbon dioxide fluxes between soil (or vegetation) and

atmosphere. Evapotranspiration and carbon dioxide fluxes of the SVAT (Soil – Vegetation –

Atmosphere) systems, have to be correctly estimated if a sustainable and parsimonious water

resources management would be made. Moreover energy and mass balances model outputs (e.g.

latent heat flux and soil moisture) can be compared with micrometeorological measurements, if

and only if micrometeorological data are rigorously processed and their qualities are assessed.

Micrometeorological technique was born about 30 years ago and, subsequently, a large

contribution about data corrections was rapidly given by many scientists. However, many

aspects about measurement proprieties and flux reliabilities are only now investigated. In the

first part of this work, starting from high frequency measurements of the three wind components

and carbon dioxide/water concentrations, eddy covariance data are processed using an open

source program and the results are compared with those obtained by a simple software

implemented at the Politecnico of Milan for averaged data for real time water management.

Thanks to this comparison the main correction procedures which have to be necessarily

implemented to obtain reliable turbulent fluxes from micrometeorological data, are shown.

The reliability of the micrometeorological measurements is usually assessed with the energy

balance closure. Moreover, the use of energy data to validate land surface models requires that

the conservation of the energy balance closure is satisfied. However, the unbalance problem is an

important issue which has not yet been resolved. In the second part of this work, many aspects

which could cause underestimation in turbulent flux measurements are shown. The factors which

could influence the energy balance colure are separately investigated and the energy balance

closure improvements or worsening are shown in order to understand the number of factors

which could play a fundament role into energy balance closure problem.

One of these problems is represented by flux scale proprieties. In fact, net radiation, latent,

sensible and ground heat fluxes (which represent the four components of the energy balance)

have different representative source areas which covers different sectors of the field: from few

centimeters for ground heat flux, to a hectare for latent and sensible heat fluxes. Therefore,

several errors in energy balance closure can be related to the difficulty to match footprint area of

eddy covariance fluxes with the source areas of the instruments which measure net radiation and

ground heat flux. In the third part of this work, representative source area for turbulent fluxes

measured by eddy covariance station is investigated through modeling and experimental

campaigns in totally different field situations: bare and vegetated soils. A revisited simple

method based on mobile and fixed eddy covariance stations is found to be helpful in intra-field

spatial variability investigations of turbulent fluxes also over homogeneous canopy such us

maize fields. The results of these experiments lead to interesting improvements about turbulent

flux representative source area knowledge increasing literature results.

This PhD thesis has been conceived as a collection of three strongly connected papers, which

constitute the nucleus of the author research activities. One introduction, at the beginning of the

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thesis, has been added to briefly explain eddy covariance technique and its mathematical basis.

The PhD thesis is subdivided in three macro chapters which are independently built in order to

simplify the comprehension of the text, giving to the reader the possibility to read each chapter

separately from each others. Each chapter is built with a quite standard structure which is

constituted by a synthetic abstract, an introduction which gives to the reader an overview about

the problems which are developed in the chapter, a theoretical background which is widely

referred to literature works, a site-instrument-data description, result discussions and finally a

conclusion remark. Other author works, which have been developed during his PhD research

period, are quoted in the text and they constitute parallel efforts which allowed completing this

thesis. Here, only the papers which have already been published are shown, while other works

which are in review or in press processes have not been quoted in the reference subparagraphs.

Subparagraph, equation and figure enumerations restart at each chapter to improve the

comprehension of the text. It is an author’s choice to use, into the equations, symbols which are

usually founded in literature articles also if they could be utilized several times into the text with

different meanings which, however, are widely explained in order to prevent any

misunderstanding.

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General Introduction

In this paragraph a theoretical background about the eddy correlation theory, with reference to

three scientific works (Baldocchi et al. (1988), Verma (1990) and Papale et al. (2006)) is shown.

It does not want to be an exhaustive dissertation about the micrometeorological method but only

a general introduction about the mathematical basis which governs the turbulent flux calculus

methodology focusing on limitations and problems connected to this approach.

Eddy covariance technique

Micrometeorological techniques provide for direct measurements of carbon dioxide, water and

energy flux exchanges between biosphere and the atmosphere. Micrometeorological techniques

have many advantages:

1) They are in situ and do not disturb the environment around the plant canopy.

2) These techniques allow continuous measurements.

3) Time averaged micrometeorological measurements at point provide an area-integrated,

ensemble average of the exchange rates between the surface and the atmosphere.

Defining as net ecosystem exchange the mass or energy quantity exchanged from ecosystem to

atmosphere trough an imaginary surface of interface in a determinate range of time, the

objectives of micrometeorological technique are:

1) To find a simple formulation about net ecosystem exchange which can be applied starting

from measurements carry out using not many expensive instruments;

2) To find a net ecosystem exchange general formulation so that the results can be

considered representative of the ecosystem behavior.

The conservation equation provides the basis framework for measuring and interpreting

micrometeorological flux measurements. In concept, the conservation equation states, which are

represented by the variation at fixed point of a chemical constituent in time, are equal to the sum

of the mean horizontal and vertical advection, mean horizontal and vertical divergence or

convergence of the turbulent flux, molecular diffusion and any source or sink as described by

Eq.1.

cScut

c 2 (1)

Where

t

c is the variation of the concentration (c) of a generic passive scalar in time;

cu

is the turbulent transport of c generated by a wind field described by the vector u

;

S is a source or sink of c in a fixed point in space;

c2 is the molecular diffusion and represents the gas diffusivity in air.

While Eq. 1 represents the instantaneous transport equation, Eq. 2 describes the evolution in time

of the mean concentration of the scalar c (Garrat, 1993).

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cScut

c 2 (2)

Applying the Reynolds’s decomposition (Foken, 2008) which converts a generic instantaneous

value as a sum of mean component and fluctuant component, in accordance with Reynolds’s

mean proprieties law, it is possible to obtain Eq. 3.

cSz

cw

y

cv

x

cu

z

cw

y

cv

x

cu

t

c 2''' (3)

Where

z

cw

y

cv

x

cu is the advection transport term generated by the mean wind flow;

z

cw

y

cv

x

cu ''' is the advection transport term generated by the turbulent flow.

Eddy correlation theory is based on ideal conditions which permit to simplify Eq. 3 in

accordance with technical objectives described before. Supposing that:

1) Molecular diffusion can be neglected in a turbulent flow;

2) Mean variation of the scalar quantity in horizontal directions can be neglected;

3) Mean vertical velocity can be neglected;

4) The turbulence is homogenous in horizontal directions;

5) The concentration of the constituent does not vary significantly with time;

it is possible to obtain Eq. 4.

z

cwS

t

c '' (4)

As described by Eq. 4, the variation of the mean concentration of gas in time is equal to the

difference between what enters or leaves the controlled volume and turbulent vertical flux.

Integrating Eq. 4 from surface to measurement height (zm) and considering the sum of what

enters or leaves the controlled volume as the net ecosystem exchange (F), it is possible to obtain

Eq. 5.

dzt

ccwF

mz

z 0

'' (5)

Eq. 5 says that the net ecosystem exchange is the sum of turbulent vertical flux and storage term.

The turbulent vertical flux is also called eddy covariance flux, while the storage term represents

gas or energy quantities which are not carried by turbulent flow and remain stored under the

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measurement point. In first approximation storage term can be neglected and Eq. 5 is simplified

in Eq. 6.

''cwF (6)

The equations of the turbulent fluxes can be summarized in:

1) Sensible heat flux (Eq. 7)

''TwCH pa (7)

2) Latent heat flux (Eq. 8)

''qwLE a (8)

3) Momentum flux (Eq. 9)

''uwa (9)

Where a is the air density, pC is the specific heat capacity of air and is the vaporization latent

heat of water. T’ represents air temperature while q’ water vapor turbulent concentration in the

atmosphere.

For other discussion on the conservation equation, as related to micrometeorological

measurements, the reader should refer to the work of Kanemasu et al. (1979) and Businger

(1986).

References

Baldocchi, D., Hincks, B., & Meyers, T. (1988). Measuring biosphere-atmosphere exchanges of biologically related

gases with micrometeorological methods. Ecology , 69: 1331-1340.

Businger, J. (1986). Evaluation of the accuracy with which dry deposition can be measured with current

micrometeorological techniques. Journal of Climate and Applied Meteorology , 25: 1100-1124.

Foken, T. (2008). Micrometeorology. Berlin: Springer, pp. 306, ISBN 978 3 540 74665 2.

Garratt, J. (1993). The atmospheric boundary layer. Cambridge: Cambridge university press, pp.316, ISBN 0 521

38052 9.

Kanemasu, E., Wesely, M., Hicks, B., & Heilman, J. (1979). Techniques for calculating energy and mass fluxes.

Michigan, USA: Pages 156-182 in B.L. Barfield and J.F.Gerber editors.

Papale, D., Reichstein, M., Aubinet, M., Canfora, E., Bernhofer, C., Kutsch, W., et al. (2006). Towards a

standardized processing of net ecosystem exchange measured with eddy covariance technique: algorithms and

uncertainty estimation. Biogeosciences , 3 : 571-583.

Verma, S. (1990). Micrometeorological methods for measuring surface fluxes of mass and energy. Remote Sensing

Reviews , 5: 99-115.

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(Chapter 1) - Impact of data corrections on turbulent flux measurements

Abstract

Reliable estimation of evapotranspiration and carbon dioxide fluxes is based on a correction

procedure due to eddy covariance methodology and instrumental characteristics. Literature

standardized methods for data processing are defined for analyzing the quality of high frequency

measurements. However, for operative applications, linked to real time irrigation water

management, high frequency data are difficult to manage. So the objective of this paper is to

verify the possibility of using eddy covariance data in an operative way in order to understand if

averaged data at 30 minutes are still of good quality in relation to those obtained from high

frequency measurements.

Data have been collected by an eddy covariance station over a maize field at Livraga (Lodi,

Italy) for the year 2012. High frequency data (20 Hz) and averaged data (30 minutes) are

collected separately in a PCMICA of 2Gb capacity and data logger memory respectively. High

frequency data are analyzed with Eddy Pro 4.0 open source software. Effects of different types

of corrections, from axis rotation to density fluctuations, are shown. Spectral correction factors

have been calculated and flux losses are estimated. Quality of corrected fluxes and energy

balance closure are also shown.

Averaged data have been analyzed with Polimi Eddy Covariance software (PEC) which accounts

only a portion of the correction procedures which can be applied to high frequency data, where

the major difference is linked to the absence of the spectra correction.

Evapotranspiration and carbon dioxide fluxes from high frequency and average data are then

compared and cumulated trends over the growing season are assessed and a small difference is

found. So these comparisons highlight the possibility of using averaged data for operative water

management without drastically decreasing the quality of fluxes.

Introduction

Energy fluxes developed in a SVAT (Soil-Vegetation-ATmosphere) system are important for a

wide range of applications at different spatial and temporal scales: from flood simulation at basin

scale to water management in agricultural areas. Reliability of eddy covariance measurements

has to be studied before using them in hydrological simulations (Aubinet et al., 2000).

Eddy covariance stations measure turbulent fluxes of sensible and latent heat, net radiation and

heat flux in the soil at agricultural field-scale, having the objective to estimate the correct water

requirement for a crop. The main instruments, which give the name to the eddy covariance

technique, are gas analyzer and tridimensional sonic anemometer. They provide for estimate

turbulent fluxes into surface layer (Stull, 1988), thanks to the covariance between vertical wind

velocity and concentration of a scalar passive (for example: air/water, temperature or carbon

dioxide). Flux estimations are obtained through complex series of steps starting from raw data

acquired with high frequencies of about 10-20 Hz. The quality of these measurements is mainly

influenced by problems of sensor configuration, place of the tower and stability of the

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atmosphere (Baldocchi, 2001; Foken and Wichura, 1996; Fuehrer and Friehe, 2002). As

described in Moncrieff at al. (1997), eddy covariance technique should be viewed as a 'system' of

measurement, i.e. which includes not only the hardware but also the method of analysis, whether

in real-time or off-line, and the algorithms used to filter or detrend the raw data and to apply

calibrations and corrections. An example of the details and considerations which are necessary in

a typical eddy covariance system is revealed in a series of papers (Shuttleworth et al., 1982,

Shuttleworth et al., 1988 Moore, 1983, Moore, 1986; Lloyd et al., 1984; Shuttleworth, 1988)

which describe not only the used instrumentation, including sensors and microcomputer control,

but also the corrections required for real-time analysis.

The problem of a correct implementation of data correction procedures is strongly connected

with micrometeorological measurements which are often not able to close the surface energy

balance equation (Foken, 2008). Uncertainties in the post-field data processing of eddy

covariance measurements of the turbulent fluxes are suspected to be crucial (Massman and Lee,

2002). Lee et al. (2004) formulate recommendations related to the eddy covariance technique for

estimating turbulent mass and energy exchange, and give a comprehensive overview on the

current state of the art regarding micrometeorological issues and methods.

Eddy Pro 4.0 is an open source software used to calculate turbulent fluxes from high frequency

measurements of wind velocity and gas concentrations. It can be founded at the WEB page

http://www.licor.com/env/products/eddy_covariance/software.html and it has been implemented

by University of Tuscia and Li-Cor industry. In recent decades, other softwares, implemented by

different universities in the world, can be found in literature (TK3, EdiRe, EddySoft, Alteddy)

with the main objective to standardize the correction procedure of eddy covariance

measurements. These softwares have been widely validated and they are all based on five

fundamental points:

1) Measured data are opportunely selected in function of quality tools;

2) Data are calibrated or corrected if necessary;

3) Data are aggregated in statistic tools as mean, variance or covariance;

4) Data are converted in averaged fluxes;

5) Reliability of fluxes is evaluated.

To provide a complete data correction procedure high frequency data are needed because they

can be used to find the reason for possible errors into flux measurements (Ueyama et al., 2012).

However, only averaged data are available sometimes (for example in real time application).

High frequency data acquisition is not practical, considering that data loggers internal memories

are not sufficient to store big quantities of data. Usually, a PCMCIA card allows expanding data

logger memory capacity, so that, high frequency data are stored on this memory card while

averaged data are stored on internal data logger memory. High frequency measurements could be

directly downloaded trough Ethernet or Wi-Fi but in many case eddy covariance system location

does not permit these types of connections. Typically through the use of GSM modem

connection data logger memory could be downloaded on a personal computer which could be

many kilometers away from the station, while the PCMCIA card has to download in situ using a

personal computer and a compact flesh reader, leading to a non operative procedure. In order to

overcome these complications, PEC software which uses directly averaged data to calculate

turbulent fluxes has been implemented (Corbari et al., 2012) and in this work comparison

between Eddy Pro 4.0 and PEC software results are shown.

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In the first part of this work, an overview of correction procedures which are necessary to obtain

reliable turbulent fluxes is described in reference to Eddy Pro 4.0. Only practical formulas are

shown, while mathematical approaches are quoted in literature. In the second part, the impact of

the various steps of post-field data processing on turbulent flux assesses is investigated. In the

third part, fluxes performed by PEC are compared to the fluxes computed by Eddy Pro 4.0 in

order to understand if reliable latent heat and carbon dioxide fluxes can still be obtained for an

operative use of irrigation water management.

Data collection

Eddy covariance data are measured by a tridimensional sonic anemometer (Young 81000) and

open path gas analyzer (LICOR 7500) located at the top of a tower 5 m high. The tower is placed

in a maize field at the city of Livraga (LO) in the Po Valley. High frequency (20 Hz)

measurements are stored in a compact flesh of 2 Gb connected with the data logger Campbell

CR5000 and downloaded in situ weekly. On compact flash only three wind velocity components,

sonic temperature, vapor and carbon dioxide concentrations are stored (raw data). Data logger

program is directly set to calculate averaged data over a time step of 30 minutes, and these data

are collected into data logger internal memory. Contemporaneously, net radiation, measured by

CNR1 Kipp&Zonen radiometer, soil heat flux, measured by HFP01 Campbell Scientific flux

plate, and soil temperature measurements are stored on data logger in different memory tables.

While high frequency data are directly used by Eddy Pro 4.0 software, 30 minutes averaged data

are the starting point for the fluxes computation using PEC software.

Experimental measurements were carried out from 21 May 2012 to 7 September 2012 but the

dataset is composed by only 3103 averaged data because some gaps due to malfunctioning of

instrumentations or rainfall days are shown into the data sequences. From 131 to 241 Julian days

the field is covered by vegetation, while the remaining days of the year, the field is characterized

by bare soil.

Preliminary processes for correction procedure

Before calculating fluxes, high frequency data have to be adjusted and if necessary neglected.

The different types of corrections are now analyzed.

Axis rotation for tilt correction

Each anemometer model adopts a customized convention for providing wind components in an

orthogonal coordinate system, so that the user is able to retrieve the actual wind direction with

respect to geographic north. Anemometer north is shown on Young 81000, by an “N” on

junction box. Wind components are indicated with u (positive if wind from East), v (positive if

wind from North), and w (positive if wind from below) and they represent x,y,z directions

respectively.

Tilt correction algorithms are necessary to correct wind statistics for any misalignment of the

sonic anemometer with respect to the local wind streamlines. In particular, this implies that

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fluxes which are evaluated perpendicular to the local streamlines are affected by spurious

contributions from the variance of along-streamlines components. Wilczak et al. (2001),

proposes three typologies of correction algorithms: double rotation, triple rotation, and the planar

fit method. For Livraga 2012 dataset a double rotation method has been used.

Double rotation method

With this method, the anemometer tilt is compensated by rotating raw wind components to

nullify the average cross-stream and vertical wind components, evaluated on the time period

defined by the flux averaging length (30 minutes). The rationale is that cross and perpendicular

wind components are averaged to zero during such time period. In the first rotation, the

measured wind vector is rotated about the z axis with objective to nullify v component.

Successively, a second rotation is performed on a new y axis with the objective to nullify w

component (for mathematical implementation of this method see Wilczak et al., 2001).

Spike removal

The so called despiking procedure consists in detecting and eliminating short term outranged

values in the time series. Following Vickers and Mahrt (1997), for each variable a spike is

detected as up to three consecutive outliers with respect to a plausibility range defined within a

certain time window, which moves throughout the time series. The rationale is that if more

consecutive values are found to exceed the plausibility threshold, an unusual physical trend can

be identified. The width of the moving window is defined as one sixth of the current flux

averaging period and the plausibile range is quantified differently for each variable. Tab. 1

provides default values used in Eddy Pro 4.0. The window moves forward half its length at a

time. The procedure is repeated up to twenty times or until no more spikes are found for all

variables. Detected spikes are counted and replaced by linear interpolation of neighboring

values.

Tab. 1. Plausibility range for spike detection for each sensitive variable.

Variable Plausibility Range

u,v Window mean +/- 3.5 standard deviation

w Window mean +/- 5.0 standard deviation

CO2,H2O Window mean +/- 3.5 standard deviation

Temperatures, Pressures Window mean +/- 3.5 standard deviation

Time lag compensation

In open path system the time lag between anemometric variables and variables measured by gas

analyzer is due to the physical distance between the two instruments, which are usually placed

several decimeters or less apart to avoid mutual disturbances. The wind field takes some time to

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travel from one instrument to the other, resulting in a certain delay between the moments the

same air parcel is sampled by the two instruments.

It is a common practice to compensate for time lags before calculating covariances between

anemometric variables and gas analyzer measurements.

In literature four different alternative methods for detecting and compensating time lags exits:

constant time lag, covariance maximization, covariance maximization with default and automatic

time lag optimization (Runkle et al., 2012; Fan et al., 1990; Eddy Pro 4.0 manual, 2012). For

Livraga 2012 dataset covariance maximization method has been used.

Covariance maximization method

The variability of wind regimes (in open path systems) suggests an automatic time lag detection

procedure, normally performed for each flux averaging period. Typically the detection is

accomplished via the covariance maximization procedure, consisting in the determination of the

time lag that maximizes the covariance of two variables, within a window of plausible time lags

(Fan et al., 1990).

Using the covariance maximization procedure a plausible time lag window has to be defined

with the minimum and maximum time lags, which constitute the end points of the plausibility

window. A too narrowed plausible window might lead to frequent use of the default (covariance

maximization with default) or either endpoint (covariance maximization) time lag, because the

actual time lag is often found to be outside the defined plausibility range. This situation leads to

systematic flux underestimations. Conversely, imposing a too broad plausibility window, the

possibility that unrealistic time lags are detected increases, especially when covariances are small

and vary erratically with the lag time. These cases often result in flux overestimations. A trade-

off must be reached between the two contrasting needs.

Detrending

Eddy correlation method of calculating fluxes requires that the fluctuating components of the

measured signals are derived by subtracting them from the mean signals. In steady-state

conditions simple linear means would be adequate, but steady state conditions rarely exist in the

atmosphere and it is necessary to remove the long term trends in the data which do not contribute

to the flux (Gash and Culf, 1996).

Different methods are described in literature for extracting turbulent fluctuations from time

series data. The most commonly applied, in the context of eddy covariance, are the block-

averaging, linear detrending (Gash and Culf, 1996) and two types of high-pass filters, namely the

moving average (Moncrieff et al., 2004) and the exponentially weighted average (McMillen,

1988; Rannik and Vesala, 1999). For Livraga 2012 data set the linear detrending is used.

Linear detrending

Gash and Culf (1996) show that it is possible to apply a linear detrend to eddy correlation data

and calculate variances and fluxes in a single pass operation, accumulating an appropriate

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16

combination of the sum of fluctuating variables and their cross products. Linear detrending

method is generally done retrospectively using a two-pass method. The data are first divided into

blocks each long normally 20-30 minutes, and a linear regression of the measured signal on time

is then calculated. The fluctuations with respect to the regression line are then calculated during

a second pass through the data. An alternative approach, proposed by Gash and Culf (1996), is to

calculate the fluxes with respect to a filtered “mean”, which is derived by feeding the measured

signal through a low-pass filter. Since this is a single pass method it can be used in real-time to

calculate the fluxes as the data are collected.

Calculating fluxes

After completing the preliminary processes, it is possible to calculate turbulent fluxes, starting

from uncorrected fluxes. Uncorrected fluxes represent gas, energy, and momentum fluxes which

are obtained by merely adjusting units of relevant covariances, in order to match the desired

output units.

This operation may imply the inclusion of some previously calculated physical parameters

described in Eddy Pro manual. These fluxes are uncorrected because some effects are not

accounted in their calculation, notably the effects of air density fluctuations, of spectral losses,

and effects of humidity on air temperature estimation through the sonic anemometer.

Uncorrected fluxes – level 0

The uncorrected fluxes are calculated according to the following equations:

1) Sensible heat flux

''0 spa TwcH (1)

2) CO2 flux, if CO2 is measured as molar density with an open path analyzer

''10 2

3

2,0 COCO dwF (2)

3) H2O flux, if H2O is measured as molar density with an open path analyzer

'' 22,0 OHOH dwF (3)

4) Latent heat flux

OHOH MFLE 22,0

3

0 10 (4)

5) Evaporatranspiration flux

OHOH MFE 22,0

3

0 10 (5)

6) Momentum flux

22

0 '''' wvwuT a (6)

Where

0H is the uncorrected sensible heat (W m-2

).

a is the air density (Kg m-3

).

pc is the air heat capacity at constant pressure (J Kg-1

K-1

).

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17

'' sTw is the covariance between turbulent vertical wind velocity ( m s-1

) and sonic temperature

(°C).

2,0 COF is the uncorrected CO2 flux (micromol m-2

s-1

)

'' 2COdw is the covariance between turbulent vertical wind velocity ( m s-1

) and moles of CO2 per

unit of volume (millimol m-3

).

OHF 2,0 is the uncorrected H2O flux (millimol m-2

s-1

).

'' 2OHdw is the covariance between turbulent vertical wind velocity ( m s-1

) and moles of H2O per

unit of volume (millimol m-3

).

0LE is the uncorrected latent heat (W m-2

).

is the latent heat of water vaporization (J Kg-1

).

OHM 2is the molecular weight of H2O (Kg mol

-1).

0E is the uncorrected evapotranspiration flux (Kg m-2

s-1

).

0T is the uncorrected momentum flux (Kg m-2

s-1

).

''wu and '' wv is the covariance between horizontal turbulent wind velocities and vertical

turbulent wind velocity, both calculated in m s-1

.

The subscript “0” indicates the level of correction.

Spectral correction factors – level 1

Spectral corrections compensate flux underestimations due to two distinct effects. The first is

referred to the fluxes which are calculated on a finite averaging time, implying that longer-term

turbulent contributions are under-sampled at some extent, or completely. The correction for these

flux losses is referred to as high-pass filtering correction because the detrending method acts

similarly to a high-pass filter, by attenuating flux contributions in the frequency range close to

the flux averaging interval. The second is connected with instrument and setup limitations that

do not allow sampling the full spatiotemporal turbulence fluctuations and necessarily imply

some space or time averaging of smaller eddies, as well as actual dampening of the small-scale

turbulent fluctuations. The correction for these flux losses is referred to as low-pass filtering

correction. Mathematical approach to calculate spectral corrections can be found in Moncrieff et

al. (1997).

For any given flux, the spectral correction procedure requires a series of conceptual steps which

can be found in Ibrom et al. (2007) and Massman (2004) works:

1) Calculation or estimation of a reference flux cospectrum, representing the true spectral

content of the investigated flux as it would be measured by a perfect system.

2) Estimation of the high-pass and low-pass filtering properties implied by the actual

measuring system and the chosen averaging period and detrending method.

3) Estimation of flux attenuation.

4) Calculation of the spectral correction factor (SCF) and application of the correction.

Spectral corrections are implemented on Livraga 2012 dataset. High-pass filtering correction is

applied following Moncrieff et al. (2004) while for low-pass filtering correction a fully analytic

method described in Moncrieff et al. (1997) is applied.

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18

SCF is defined as the ratio between the integral of theoretical cospectrum model and the integral

of measured co spectrum (Moncrieff et al., 1997). Measured co spectrum can be obtained

starting from theoretical co spectrum multiplied for a transfer function which describes the

proprieties of the measurement system (Eq. 7).

dffTfCo

dffCoSCF

F

Theo

i

Theo

i

i)()(

)( (7)

Where Theo

iCo is the theoretical co spectrum of the flux i, FT is the transfer function and f is the

frequency. SCF is always major of 1 because it has to compensate flux underestimations caused

by the problems described in section 4.2. The most widely used theoretical co spectral models

are those from Kaimal et al. (1972). Moore (1986) proposes a scheme whereby a series of

transfer functions could be defined for each of the correction terms required in an eddy

covariance system. The transfer function defines the system reliance on different factors as

digital recursive running mean, dynamic frequency response of the sensors, sensors response

mismatch, scalar path averaging and so on, each connected with the typology of anemometer and

gas analyzer used on the eddy covariance tower (Massman, 2000).

Starting from SCF, it is possible to calculate the fractional error on the measured flux as Eq.8

(Moncrieff et al., 1997).

1001

1(%)i

iSCF

lossFlux (8)

Where Flux loss defines the whole system flux losses.

Spectral corrections are applied first to open path fluxes. This is because sensible and latent heat

fluxes used in the Webb-Pearman-Leuning (WPL) correction (Webb et al., 1980) are the

“environmental ones”, those actually present in the atmosphere and affecting measurements of

molar densities in open path analyzer.

Marking as 1 the fluxes obtained after spectral corrections, CO2, H2O latent heat and

evapotranspiration fluxes are described by Eq. 9, Eq. 10, Eq. 11 and Eq.12 respectively.

2,2,02,1 COwCOCO SCFFF (9)

OHwCOOH SCFFF 2,2,02,1 (10)

OHwSCFLELE 2,01 (11)

OHwSCFEE 2,01 (12)

Where 2,COwSCF and OHwSCF 2, are the spectral correction factors calculated for CO2 and H2O

respectively.

Furthermore, uncorrected momentum flux is corrected using the relevant spectral correction

factor wuSCF , (Eq. 13).

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19

wuSCFTT ,01 (13)

Corrected fluxes – level 2 and 3

After the spectral correction, evapotranspiration flux is at first corrected with the WPL term,

following the formulation proposed in Webb et al. (1980) (Eq.14).

apa

w

Tc

HEE 0

12 )1()1( (14)

Where

is the ratio between molar density of dry air and molar density of the water ( non

dimensional).

is the water to dry air density ratio (non dimensional).

aT is the ambient air temperature (°C).

wis the water density (Kg m

-3).

Sonic temperature and sensible heat flux are corrected for humidity effects following van Dijk et

al. (2004), revising Schotanus et al. (1983) (Eq. 15). In next sections, this correction is simply

called VD.

''202 s

a

spa TwQE

TcHH (15)

Where is a constant equals to 0.51 and Q is the specific humidity (non dimensional).

H2 is then spectrally corrected to get the first fully corrected flux (Eq. 16).

TswSCFHH ,23 (16)

Where TswSCF , is the spectral correction factor calculated for sonic temperature. When CO2 and

H2O molar densities are measured with an open path gas analyzer in cold environmental (with

low temperature below -10 °C) H0 has to be corrected to account for the additional instrument-

related sensible heat flux, due to instrument surface heating/cooling. This correction is fully

described and tested in literature (Burba et al., 2008).

Now that sensible heat is fully corrected, evapotranspiration flux is corrected again, adding the

WPL terms with the revised H (Eq. 17).

apa

w

Tc

HEE 3

13 )1()1( (17)

Water vapor and latent heat fluxes are easily determined:

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20

OHOH MEF 23

3

2,3 10 (18)

33 ELE (19)

Now that evapotranspiration and sensible heat fluxes are fully corrected, fluxes of other gases

such as carbon dioxide can be corrected for air density fluctuations, according to Webb et al.

(1980). For carbon dioxide we get the Eq. 20.

apa

CO

d

COCOCO

Tc

dHC

dEBFAF 232

12,12,2 1 (20)

Where A, B and C are multipliers described in Webb et al. (1980). Finally, corrected fluxes of

CO2 (F3,CO2) in a system with open path instrument, coincide with fluxes at level 2.

Results

As shown in the previous paragraphs, correction procedures can be summarized in three groups:

preliminary processes, spectral corrections, WPL and VD corrections. In this section the impact

of correction procedures in half-hourly measurements is quantified. With the expectation of the

corrected fluxes calculation, results of the standardized processing procedure described above

are performed. In general, to quantify the impact of each correction procedure, the slope and

intercept values between the post-processed fluxes and pre-processed fluxes from a regression

analysis on half hourly basis, have been calculated. The slope represents a difference in

proportion to flux magnitude, and the intercept represents a constant difference on all flux range.

Effect of the preliminary processes on raw data

Preliminary processes should be applied on raw data measurements to prepare the dataset for

fluxing calculation. In Fig.1 the effect of different correction methods on each u, v, w, H2O and

CO2 averaged component is shown.

A B

-6

-4

-2

0

2

4

6

218 218.2 218.4 218.6 218.8 219

Win

d v

elo

city

(m

s-1

)

Julian day

u (raw data)

u (raw data+despiking+double

rotation+time lag+detrending)

0

200

400

600

800

1000

1200

1400

215 215.2 215.4 215.6 215.8 216

Ga

s co

nce

ntr

ati

on

(m

illi

mo

l m

-3)

Julian day

H2O (raw data)

H2O (raw data+despiking+double

rotation+time lag+detrending)

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21

C D

-6

-4

-2

0

2

4

6

218 218.2 218.4 218.6 218.8 219

Win

d v

elo

city

(m

s-1

)

Julian day

v (raw data)

v (raw data+despiking+double

rotation+time lag+detrending)

5

10

15

20

25

30

227.5 227.7 227.9 228.1 228.3 228.5

Ga

s co

nce

ntr

ati

on

(m

illi

mo

l m

-3)

Julian day

CO2 (raw data)

CO2 (raw data+despiking+double

rotation+time lag+detrending)

E

-0.4

-0.3

-0.2

-0.1

0

0.1

218 218.2 218.4 218.6 218.8 219

Win

d v

elo

city

(m

s-1

)

Julian day

w (raw data)

w (raw data+despiking+double

rotation+time lag+detrending)

Fig. 1. Effects of the preliminary correction methods on wind velocities (A, C, E) and gas

concentrations (B, D).

Double rotation method produces a modification of the anemometer coordinate system (x,y,z) in

respect to the local wind streamlines. The consequence of these rotations is that v and w wind

components are led to zero (Fig. 1C and E) while u turns out to be characterized only by positive

terms (Fig. 1A). This effect is also shown Fig. 2A where the dots, which represent modulus of u

after double correction, take place only in first and fourth sectors. The effect of double rotation is

major in correspondence of weak wind intensity. The modulus of u is subject to slight variations

in a range of wind velocity between -3 m s-1

and 3 m s-1

; while no variation are present for high

values of modulus of u, and the dots stay on bisectors of first and fourth sectors (grey line). CO2

and H2O concentrations are not particularly affected by preliminary corrections procedures (Fig.

2B and C), and only in correspondence of the raw data peaks, data corrections are relevant (Fig.

1B and D). This behavior could be a good indicator of the reliability of the gas analyzer

measurements. In fact, calculating over the experimental period the mean differences between

CO2 and H2O raw data concentrations and CO2 and H2O corrected concentrations (after the

application of the preliminary processes), the results are quite similar and equal to -0.0274

millimol m-3

and 0.118 millimol m-3

respectively.

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22

A B

0

1

2

3

4

5

6

7

8

9

-8 -6 -4 -2 0 2 4 6 8

u -

win

d c

orr

ecte

d v

elo

city

(m

s-1

)

u - wind raw data velocity (m s-1)

0

200

400

600

800

1000

1200

1400

1600

0 200 400 600 800 1000 1200 1400 1600

H2O

co

rrec

ted

co

nce

ntr

ati

on

(mil

lim

ol

m-3

)

H2O raw data concentration (millimol m-3) C

0

5

10

15

20

25

30

35

40

0 5 10 15 20 25 30 35 40

CO

2co

rrec

ted

co

nce

ntr

ati

on

(mil

lim

ol

m-3

)

CO2 raw data concnetration (millimol m-3)

Fig. 2. Comparison between mean raw data of u (A), H2O (B) and CO2 (C) concentrations before

and after preliminary correction procedures.

Effect of the preliminary processes on uncorrected fluxes

When fluxes directly obtained by raw data covariances and those calculated after preliminary

processes (uncorrected – level 0) are compared, slight differences are found, and in Fig.3 the

results are shown. The differences are quantified as slope between uncorrected fluxes and raw

data fluxes from a regression analysis on half-hourly basis. The (1-slope) and intercepts

quantities measure the difference in flux magnitude after the application of correction procedure

while R2 represents the dots dispersion around the regression line which describes the

amplification of the random error (Ueyama et al., 2012).

A

0.20

0.40

0.60

0.80

1.00

1.20

0.20

0.40

0.60

0.80

1.00

1.20

FH2O FCO2 LE H

R2

(-)

Slo

pe

(-)

Slope

R2

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23

B C

-2.40

-2.00

-1.60

-1.20

-0.80

-0.40

0.00

0.40

FH2O FCO2*

Inte

rcep

t (m

illi

mo

l m

-2s-1

)

-6.00

-4.00

-2.00

0.00

2.00

4.00

LE H

Inte

rcep

t (W

m-2

)

Fig. 3. A. Slope and R2 determined by regression of half-hourly fluxes before and after

preliminary corrections. B and C. Intercepts of the regression lines. In FCO2* the intercept is

represented as (millimol m-2

s-1

)103.

As shown in Fig. 3A, preliminary corrections produce a decrease of flux intensities which varies

from 8% for latent heat and H2O to 36% for CO2. Only sensible heat has a slight increase of

about 6%. For momentum flux (not shown in figure) slope is equal to 0.86 while intercept is

about -0.01 Kg m-2

s-1

, therefore preliminary processes produce a decrease of about 14% in its

flux magnitude. Evaluating mean slope performed over the whole preferable fluxes (from vapor

to momentum), the preliminary corrections produce a decrease of turbulent flux intensities of

about 12%. R2 deviates from 1 of about 18% on all fluxes, except for CO2 where R

2 is equal to

0.47, indicating that, for this flux, application of preliminary processes create random error

amplification. Moderated shifts of turbulent flux mean intensities are shown Fig.3B and C,

where the range of intercept values vary from -5 W m-2

for sensible heat to 1.71 W m-2

for latent

heat. For CO2 flux the intercept is equal to -2.3 micromol m-2

s-1

while for H2O flux preliminary

processes do not play a substantial role in the alteration of its mean intensity.

As shown in Fig. 4, where the trend of fluxes over an experimental day is shown, spike removal

correction leads to the elimination of some peaks of data. However, the remaining peaks in the

flux series may be due to particular physical phenomena related with atmospheric or field events.

A B

-100

-80

-60

-40

-20

0

20

40

60

80

100

217 217.2 217.4 217.6 217.8 218

CO

2fl

ux

(m

icro

mo

l m

-2s-1

)

Julian day

Fo,CO2 (from raw data)

Fo,CO2 (uncorrected)

-30

-20

-10

0

10

20

30

217 217.2 217.4 217.6 217.8 218

H2O

flu

x (

mil

lim

ol

m-2

s-1)

Julian day

Fo,H2O (from raw data)

Fo,H2O (uncorrected)

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24

C D

-200

-100

0

100

200

218.0 218.2 218.4 218.6 218.8 219.0

Sen

sib

le h

eat

flu

x (

W m

-2)

Julian day

Ho (from raw data)

Ho (uncorrected)

-500

-250

0

250

500

218.0 218.2 218.4 218.6 218.8 219.0

La

ten

t h

eat

flu

x (

W m

-2)

Julian day

LEo (from raw

data)

Fig. 4. Comparison between mean raw data fluxes before and after preliminary correction

procedures.

Effect of the spectral corrections on turbulent fluxes

n Fig.5, spectral correction impact over uncorrected turbulent fluxes is shown. In this case, slope

represents the ratio between fluxes at level 1 and fluxes at level 0. Only for sensible heat the ratio

is calculated between H3 and H2 because the spectral correction is applied after the WPL and VD

equations. Spectral correction factor is a value always greater than 1, and this produce, on all

turbulent fluxes (including momentum flux), a systematic growth in slope of about 10%

(Fig.5A). The regression coefficient (R2) is closed at about 0.99 on all fluxes. The maximum

intercept values are in correspondence with CO2 and latent heat fluxes where the difference

before and after the application of the spectral correction is equal to 0.61 micromol m-2

s-1

and

0.60 W m-2

respectively (Fig. 5B and C), while H2O and sensible heat intercepts are near to zero.

A

0.8

0.9

1.0

1.1

1.2

0.6

0.8

1

1.2

1.4

FH2O FCO2 LE H

R2 (-)

Slo

pe

(-)

Slope

R2

B C

0

0.2

0.4

0.6

0.8

FH2O FCO2*

Inte

rcep

t (m

illi

mo

l m

-2s-1

)

0

0.2

0.4

0.6

0.8

LE H

Inte

rcep

t (

W m

-2)

Fig. 5. A. Slope and R2 calculated by regression of half-hourly fluxes before and after the application of SCF on uncorrected

fluxes. B and C. Intercepts of the regression lines. In FCO2* the intercept is represented as (millimol m-2 s-1

) 103.

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25

In the next sessions flux losses for the whole range of turbulent fluxes are investigated with the

objective to understand if some atmospheric or turbulent characteristics could influence the

spectra or cospectra information losses. In Fig. 6 the flux losses (for water vapor, carbon dioxide,

latent heat, sensible heat and momentum fluxes), in function of the main atmospheric proprieties,

are shown.

Flux loss in function of air temperature and relative humidity

Minimum value of flux loss for momentum and sensible heat is about 0.7% while maximum

value of flux loss is about 30%. For latent heat, CO2 and H2O minimum flux loss is about 7%

while the maximum flux loss is about 87%. This is probably due to the proprieties of transfer

function ( FT ) which is calculated as a product of different transfer functions connected with

characteristics of the systems used to measure eddy covariance variables (Moore, 1986).

Sensible heat and momentum fluxes can be calculated starting only from data measured by sonic

anemometer instrument, so that transfer function has to take into account only anemometer

signal losses. Instead, latent heat, H2O and CO2 fluxes are calculated using sonic anemometer

and gas analyzer contemporaneously. In this case, the transfer function has to take into account

flux information losses derived by anemometer and gas analyzer with a consequent rising in the

turbulent flux loss. For all fluxes, the flux loss is not particularly influenced by air temperature.

In general, a random distribution of the dots is shown in correspondence with a range of

temperature which varies from 10 °C to 30 °C. Major dispersion of dots is shown in association

with latent heat, CO2 and H2O fluxes with a standard deviation in flux loss of about 9%. Air

humidity plays a modest role on flux loss. For high values of relative humidity, dispersion of

dots and flux loss tend to increase up to maximum values of 30% (for sensible heat and

momentum fluxes) and 87% (for latent heat, H2O and CO2 fluxes). As shown in Runkle et al.

(2012), relative humidity plays a fundamental role on time lag of close-path gas analyzers, where

the time lag is a parameter included in the transfer function implementation (Massman, 2000).

Fig. 6 results show that high air humidity concentrations (also in an open path gas analyzer)

could influence transfer function with a consequent increase in flux loss.

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26

Mo

men

tum

flu

x

Sen

sib

le h

eat

Lat

ent

hea

t

CO

2 f

lux

H2O

flu

x

Air Temperature Relative humidity Wind velocity Friction velocity Stability parameter

Fig. 6. Flux loss in function of atmospheric characteristics.

0

10

20

30

40

50

60

70

80

90

10

0

05

10

15

20

25

30

35

Flux loss (%)

Air

te

mp

era

ture

(C

)

0

10

20

30

40

50

60

70

80

90

10

0

05

10

15

20

25

30

35

Flux loss (%)

Air

te

mp

era

ture (

C)

0102030405060708090100

05

1015

2025

3035

Flux loss (%)

Air

te

mp

era

ture

(C

)

0

10

20

30

40

50

60

70

80

90

10

0

05

10

15

20

25

30

35

Flux loss (%)

Air

te

mp

era

ture

(C

)

0

10

20

30

40

50

60

70

80

90

10

0

01

02

03

04

05

06

07

08

09

01

00

Flux loss (%)

Rea

ltiv

e h

um

idit

y (%

)0

10

20

30

40

50

60

70

80

90

10

0

01

02

03

04

05

06

07

08

09

01

00

Flux loss (%)R

ealt

ive

hu

mid

ity

(%

)

0102030405060708090100

010

2030

4050

6070

8090

100

Flux loss (%)

Rea

ltiv

e h

um

idit

y (%

)

0

10

20

30

40

50

60

70

80

90

10

0

01

02

03

04

05

06

07

08

09

01

00

Flux loss (%)

Rea

ltiv

e h

um

idit

y (%

)

0

10

20

30

40

50

60

70

80

90

10

0

01

02

03

04

05

06

07

08

09

01

00

Flux loss (%)

Rea

ltiv

e h

um

idit

y (%

)

0.11

10

10

0

02

46

81

0

Flux loss (%)

Win

d v

elo

city

(m

s-1

)0

.11

10

10

0

02

46

81

0

Flux loss (%)

Win

d v

elo

cit

y (m

s-1

)110100

02

46

810

Flux loss (%)

Win

d v

elo

city

(m s

-1)

1

10

10

0

02

46

81

0

Flux loss (%)

Win

d v

elo

city

(m

s-1

)

1

10

10

0

02

46

81

0

Flux loss (%)

Win

d v

elo

city

(m

s-1

)

1

10

10

0

00

.51

1.5

2

Flux loss (%)

Fri

ctio

n v

elo

city

(m

s-1

)1

10

10

0

00

.51

1.5

2

Flux loss (%)

Fri

ctio

n v

elo

city

(m

s-1

)

110

10

0

00

.51

1.5

2

Flux loss (%)

Fri

ctio

n v

elo

city

(m

s-1

)

0.11

10

10

0

00

.51

1.5

2

Flux loss (%)

Fric

tio

n v

elo

cit

y (

m s

-1)

0.11

10

10

0

00

.51

1.5

2

Flux loss (%)

Fri

ctio

n v

elo

city

(m

s-1

)

0

10

20

30

40

50

60

70

80

90

10

0

-50

-30

-10

10

30

50

Flux loss (%)

Sta

bil

ity

pa

ram

eter

(-)

0

10

20

30

40

50

60

70

80

90

10

0

-50

-30

-10

10

30

50

Flux loss (%)

Sta

bil

ity

pa

ra

mete

r (-)

010

2030405060708090

10

0

-50

-30

-10

103

050

Flux loss (%)

Sta

bil

ity

pa

ram

eter

(-)

0

10

20

30

40

50

60

70

80

90

10

0

-50

-30

-10

10

30

50

Flux loss (%)

Sta

bil

ity

pa

ram

eter

(-)

0

10

20

30

40

50

60

70

80

90

10

0

-50

-30

-10

10

30

50

Flux loss (%)

Sta

bil

ity

pa

ram

eter

(-)

0

10

20

30

40

50

60

70

80

90

10

0

05

10

15

20

25

30

35

Flux loss (%)

Air

te

mp

era

ture

(C

)

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27

Flux loss in function of wind velocity and friction velocity

In Po Valley wind velocity intensities are not particularly elevated. During unfavorable weather

conditions maximum velocities can be up to about 10 m s-1

. As shown in Moncrieff et al. (1997),

low wind speed, which favors a greater proportion of large eddies, produces a flux

underestimation. In Fig. 6 graphs of flux loss in function of wind velocity and friction velocity

are shown in a semi logarithmic Cartesian plane to highlight the negative effect of slow wind

velocities. For wind velocities of about 2.5 m s-1

, flux loss tends to be stabilized at about 10%.

Analyzing the trend with wind velocities higher than 4 m s-1

, flux underestimation tends to

increase slightly in a linear way. However, the experimental design for a limited range of wind

intensity does not permit to understand if also high velocities could add flux losses. Moncrieff et

al. (1997) show that in a close-path gas analyzer, errors occur with high wind speed and when

the instruments are near the ground leading to a flux loss up to 40% with a wind velocity of

about 8 m s-1

. Even if an open path anlyzer is a completely different instrument in respect to a

close path, it is constituted as well by an optical window which should modify wind flow during

its passage through it with a consequent slight increase of information loss.

Friction velocity is a characteristic parameter of mechanical turbulence (Foken, 2008).

Turbulence is an important issue connected with the correct measurement obtained by eddy

covariance stations. Eddy covariance technique is based on measurement of wind and gas

concentrations turbulent variables in atmospheric surface layer (Foken, 2008; Garrat, 1993).

Laminar flows or advection conditions represents negative situations where the eddy covariance

station is not able to measure correctly fluxes. As shown in Fig.6, for small values of friction

velocity, flux loss increases drastically. In many different literature works (Aubinet et al., 2000;

Falge et al., 2001), friction velocity is used as a threshold which indicates the level of turbulence

in a site. Reichstein et al. (2002) assumes that all eddy covariance data with u* < 0.2 m s-1

should

be excluded from the analysis, as it is likely that under these conditions storage and advection

can reduce gas fluxes through the boundary layer. However, as shown in Barr et al. (2006), 0.2

m s-1

can not be used as a universal threshold value, but it has to be estimated starting from

micrometeorological parameters measured by the tower at each site. From results shown in Fig.

6, optimal u* threshold definition could not be individuated. To provide the u* threshold, Papale

et al. (2006) method should be applied but, it is not an objective of this work.

Flux loss in function of stability parameter

Stability parameter is defined as the ratio between measurement height (taking into account

about displacement height) and Monin-Obukhov length (Obukhov, 1946). It is a dimensionless

parameter that characterizes turbulent processes in the surface layer, and it is described by Eq.21.

L

dz )( (21)

Where

is the stability parameter (non dimensional).

z is the measurement height (m)

Page 28: EDDY COVARIANCE MEASUREMENTS IN THE PO VALLEY ... · EDDY COVARIANCE MEASUREMENTS IN THE PO VALLEY: REPRESENTATIVENESS AND ACCURACY Chair of the doctoral program: Prof. Fernando Sansò

28

d is the displacement height described in Foken (2008) (m).

L Monin-Obukhov length (m).

Monin-Obukhov length is defined as the ratio between mechanical and convective forces as

shown in Eq. 22.

''

*3

Twkg

uTL a (22)

Where

Ta is the main air temperature (K).

u* is the friction velocity (m s-1

).

k is the Von Karman constant (0.4) (non dimensionaless).

g is the gravity acceleration (m s-2

).

Starting from Monin-Obukhov length, it is possible to define if the atmosphere is in convective,

stable or adiabatic conditions (Foken, 2008). When L<0 ( ''Tw >0 and 0 ) atmosphere is in a

convective condition, L>0 ( ''Tw <0 and 0 ) atmosphere is in a stable condition and |L| =

( ''Tw and tend to 0) atmosphere is in adiabatic condition.

Spectral and co spectral theoretical models are described with different formulations respect to

the stability characteristics of the atmosphere (Kaimal et al., 1972) and, as a consequence of this

reason, stability parameter plays an important role on flux loss with a substantial difference

between stable or convective conditions. As shown in Fig. 6, during convective conditions flux

loss is constant (about 8%), while in stable conditions flux loss tends to increase rapidly (up to

80%). That being so, turbulence generated by convective and mechanical forces

contemporaneously is necessary to guarantee a minimum flux loss. Starting from all

experimental data set, assuming that convective conditions is verified when 1.0 , stable

conditions when 1.0 and near adiabatic conditions when 1.01.0 (Foken, 2008), 43%

of data is in convective conditions, 33% in stable conditions and 25% is in adiabatic conditions.

Daily and seasonal trend of flux losses

In Fig. 7 daily and seasonal trend of flux losses are shown. During daytime the averaged flux

losses are smaller than night time of about 10% (Fig. 7A). From 6 A.M. to 18 P.M. for latent

heat, carbon dioxide and air vapor fluxes, flux loss is about 8%. Form 18 P.M. to 6 A.M. the flux

loss is about 17%. Considering the effect of stability conditions on flux losses, these results are

in accordance with those obtained in many literature works and in Masseroni et al. (2011) which,

starting from eddy covariance data sets measured in Landriano and Livraga in the year 2011,

shows that convective situations are prevalent during day time while in the night time the stable

conditions are dominant. Sensible heat and momentum fluxes are characterized by a small flux

loss of about 2% for the entire day. This marked difference in flux loss between latent heat,

carbon dioxide, air vapor fluxes and sensible heat, momentum fluxes is probably due to the

proprieties of the transfer functions. Combination of several instruments to measure a flux give a

contribute to increase flux loss.

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29

A peak of flux loss (of about 15% for latent heat, CO2 and H2O fluxes) is located at July but, as

shown in Fig. 7B, a seasonal trend is not definable.

A B

0

2

4

6

8

10

12

14

16

18

20

0-6 6-12 12-18 18-24

Flu

x lo

ss (

%)

Time (h)

Momentum flux

Sensible heat flux

Latent heat flux

Carbon dioxide flux

Water vapour flux

0

2

4

6

8

10

12

14

16

18

20

Flu

x lo

ss (

%)

Momentum flux

Sensible heat flux

Latent heat flux

Carbon dioxide flux

Water vapour flux

Fig. 7. Daily (A) and seasonal (B) trends of flux losses.

Effect of the WPL and VD corrections on fluxes at level 3

After the application of the preliminary processes and spectral corrections, turbulent fluxes need

to be corrected for density fluctuation and humidity effects trough the WPL and VD algorithms

(Leuning, 2004). VD correction impact on sensible heat (Eq. 15) produces a decrease in its

uncorrected value (H0) as a consequence of the humidity effect on sonic temperature, while WPL

correction is an additive terms for the uncorrected fluxes of latent, vapor and carbon dioxide as

shown by Eq. 14 and Eq. 20.

All flux estimations, with the exception of momentum flux, change in magnitude after the

application of these corrections (as shown in Fig. 8A). The slope is calculated as the ratio

between corrected fluxes at level 3 and fluxes at level 1 (after the spectral corrections), while for

sensible heat the ratio is performed between H2 and H0. From H2O flux to latent heat, an

important increase in magnitude of fluxes is caused by WPL correction, while for sensible heat

VD correction produces a decrease of the mean intensity. Magnitude of the differences is about

20% for H2O, CO2 and latent heat, while for sensible heat the examined difference is about -

15%. A constant increase of flux is presented in CO2 terms where the intercept is 2.2 micromol

m-2

s-1

(Fig. 8B). On the contrary, sensible heat is subjected to a decreasing of flux of about -4 W

m-2

(Fig. 8C).

A

0.8

0.9

1

1.1

1.2

0.8

1

1.2

1.4

FH2O FCO2 LE H

R2(-

)

Slo

pe(-

)

Page 30: EDDY COVARIANCE MEASUREMENTS IN THE PO VALLEY ... · EDDY COVARIANCE MEASUREMENTS IN THE PO VALLEY: REPRESENTATIVENESS AND ACCURACY Chair of the doctoral program: Prof. Fernando Sansò

30

B C

0

0.6

1.2

1.8

2.4

FH2O FCO2*

Inte

rcep

t (m

illi

mo

l m

-2s-1

)

-5.6

-3.6

-1.6

0.4

2.4

LE H

Inte

rcep

t (W

m-2

)

Fig.8. A. Slope and R2 calculated by regression of half-hourly fluxes before and after the

application of WPL and VD corrections on fluxes at level 1. B and C. Intercepts of the regression

lines. In FCO2* the intercept is represented as (millimol m-2

s-1

) 103.

To quantify the impact of WPL and VD corrections over the whole experimental days,

cumulated evapotranspiration and carbon dioxide fluxes are calculated, and the results are shown

in Fig. 9. Impact of correction procedures, which permit to obtain reliable values of turbulent

fluxes, is shown taking into account the divergence between fluxes at level 1 and the corrected

fluxes. At the end of the growing season, uncorrected evapotranspiration results are

underestimated with respect to corrected fluxes with a difference of about 34 mm (Fig. 9A).

After a brief period of time where CO2 cumulated flux is positive, due to the absence of

vegetation in the field, plant photosynthesis effects play an essential role in the reduction of CO2

concentration in the air (Fig. 9B). Correction procedures permit to estimate correctly CO2

cumulated flux which is distant from uncorrected flux of about 443 g m-2

. If the WPL and VD

corrections are not applied, CO2 sequestration is overestimated. Another important issue

connected with the necessity to apply the WPL and VD corrections for the correct estimation of

CO2 flux, is shown in reference with the first period of growing season which come from 140 to

160 Julian days. This period of time, which is characterized by a heterogeneous surface, fluxes

between soil and atmosphere are exchanged. When the vegetation is sufficiently high to cover

completely the soil, respiration effects, characteristics of a bare soil, are substituted by

photosynthesis processes produced by the vegetation. If WPL and VD corrections are not

applied, physical process of respiration that occurs in the first part of growing season is not

evidenced with a drastic consequence over the physical interpretation of the flux measurements.

A B

0

50

100

150

200

250

300

140 160 180 200 220 240 260

Ev

ap

otr

an

spir

ati

on

(m

m)

Julian day

ET_uncorrected

ET_corrected

-1.8E+03

-1.5E+03

-1.2E+03

-9.0E+02

-6.0E+02

-3.0E+02

0.0E+00

3.0E+02

140 160 180 200 220 240 260

CO

2cu

mu

late

d f

lux

(g

m-2

)

Julian day

CO2_uncorrected

CO2_corrected

Fig. 9. Evapotranspiration (A) and carbon dioxide (B) cumulated fluxes over growing season.

Page 31: EDDY COVARIANCE MEASUREMENTS IN THE PO VALLEY ... · EDDY COVARIANCE MEASUREMENTS IN THE PO VALLEY: REPRESENTATIVENESS AND ACCURACY Chair of the doctoral program: Prof. Fernando Sansò

31

Quality of fluxes

Quality of fluxes is evaluated through two different automatic tests implemented in Eddy Pro

4.0: statistical tests applied directly on high frequency measurements (Vickers and Mahrt, 1997)

and micrometeorological tests (Foken et al., 2004; Mauder and Foken, 2004).

Statistical screen for high frequency data is obtained applying six statistical tests described in the

work of Vickers and Mahrt (1997): spike, amplitude resolution, drop-out, absolute limits,

discontinuities, skewness and kurtosis.

Family of micrometeorological tests is constituted by two tests which are known as steady state

test and developed turbulent conditions test (Foken et al. 2004; Foken and Wichura, 1996;

Gockede et al., 2008). As described in Foken and Wichura (1996) stationary test and developed

turbulence test are summarized in a classification scheme defined above 9 levels of averaged

data quality. 1 corresponds to good quality, 9 bad quality of data which should be discarded from

the dataset. In Mauder and Foken (2004), quality of fluxes is based on a flag which can be 0, 1 or

2 from best quality to worst quality respectively. 0 quality flag corresponds with a range of

steady state and developed turbulence test levels which vary from 1 to 2; 1 quality flag

corresponds with a range which is up to 5 and 2 quality flag corresponds with a range from 6 to

7. Eddy Pro 4.0 shows these flags in association with each flux value (latent, sensible heat,

momentum and carbon dioxide flux) in order that the user can decide if the flux should be

discarded from results dataset.

Steady state test is based on idea to compare covariances determined for an averaging period

with the same parameters evaluated in short intervals within this period, using the method

explained in Gurjanov et al. (1984). A time series is considered to be in steady state if the

difference between both covariances (that are the covariance calculated over whole period and

the mean of covariances obtained in short intervals within this period) is lower 30% (Foken and

Wichura, 1996). In Fig. 10A, frequency of '','','' 2COwTwuw s and '' 2OHw covariance data for

each degree of quality, are shown. About 45% of data are included in 1 degree of quality

highlighting the good agreement of quality of measurements in respect to the stationary

condition control. From class 2 to 6 there are about 10% of data (for each class) and from class 7

to 9 about 5% of data.

A B

0

10

20

30

40

50

60

1 2 3 4 5 6 7 8 9

Fre

qu

ency

(%

)

Degree of quality

Stationary test (Foken and Wichura, 1996)

w/u

w/Ts

w/CO2

w/H2O

0

10

20

30

40

50

60

1 2 3 4 5 6 7 8 9

Fre

qu

ency

(%

)

Degree of quality

Developed turbulence test (Foken and Wichura, 1996)

u

w

Ts

Fig. 10. Percentage of data for each degree of quality using two different tests: stationary test (A)

and developed turbulent test (B).

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32

The so called flux variance similarity, which is explained in many textbooks as Foken (2008), is

a good measure to test the development of turbulent conditions. This similarity means that the

ratio of standard deviation of a turbulent parameter and its turbulent flux is nearly constant or

function of the stability conditions of atmosphere through Monin-Obukov length parameter and

measurement height. This ratio called integral turbulence characteristic (ITC) is the basic

parameter to describe atmospheric turbulence. Foken (1991) classify ITC functions in three

groups related to u, w and Ts parameters, and a well developed turbulence can be assumed if the

modulus of relative error between modeled ITC and measured ITC is lower than 30%. In Fig.

10B frequency of ITCu, ITCw and ITCTs values for each degree of quality are shown. The results

evidence a discrete percentage of data (about 15%) which stay in class 9 of quality, showing that

well developed turbulence is not always guarantee.

Assuming the Mauder and Foken (2004) classification of data quality (Fig. 11) about 25% of

turbulent fluxes over the total data set should be neglected because they are included in the class

2 of quality sectors. This is probably due to the fact that, in general, nighttime data are flagged

because developed turbulence test is failed while during dawn and dusk the steady test fails.

0

10

20

30

40

50

60

0 1 2

Fre

qu

ency

(%

)

Degree of quality

Quality test (Mauder and Foken, 2004)

H

LE

CO2_flux

Fig. 11. Percentage of data for each quality class using Mauder and Foken (2004) quality test.

In Fig. 12, turbulent fluxes are shown using dots with different shape in relation with their

quality class. Bad quality of data is shown mainly during night time, while during day time the

fluxes measured by eddy station can be considered of good quality. Dawn and dusk represent

intermediate conditions where it is not always possible to define the good or bad quality of data.

A B

-100

-50

0

50

100

150

200

227 227.5 228 228.5 229

Sen

sib

le h

eat

flu

x (

W m

-2)

Julian day

0_(good quality)

1_(sufficient quality)

2_(bad quality)

-100

0

100

200

300

400

500

227 227.5 228 228.5 229

La

ten

t h

eat

flu

x (

W m

-2)

Julian day

0_(good quality)

1_(sufficient quality)

2_(bad quality)

Page 33: EDDY COVARIANCE MEASUREMENTS IN THE PO VALLEY ... · EDDY COVARIANCE MEASUREMENTS IN THE PO VALLEY: REPRESENTATIVENESS AND ACCURACY Chair of the doctoral program: Prof. Fernando Sansò

33

C

-60

-40

-20

0

20

40

227 227.5 228 228.5 229

CO

2fl

ux

(m

icro

mo

l m

-2s-1

)

Julian day

0_(good quality)

1_(sufficient quality)

2_(bad quality)

Fig. 12. Turbulent fluxes representation in function of their quality class. (A) Sensible heat. (B)

Latent heat. (C) Carbon dioxide flux.

Quality of data is strongly connected with atmospheric stability as shown in Fig. 13. Data are

subdivided in convective, adiabatic and stable conditions and their quality flag has been

examined. The results shown in Fig. 13 indicate that the bad quality of fluxes is mainly

concentrated during stable condition of the atmosphere while for adiabatic and convective

situations quality of fluxes is often guaranteed. However, it is not possible to eliminate

completely fluxes in stable conditions because it should cause a loss of data of about 10%,

calculated as the sum of stable fluxes which belong to 0 and 1 quality classes.

A B

0

10

20

30

40

01

2

Fre

qu

ency

(%

)

Degree of quality

Quality test for sensible heat flux

Convective

Adiabatic

Stable

0

10

20

30

40

01

2

Fre

qu

ency

(%

)

Degree of quality

Quality test for latent heat flux

Convective

Adiabatic

Stable

C

0

10

20

30

40

01

2

Fre

qu

ency

(%

)

Degree of quality

Quality test for CO2 flux

Convective

Adiabatic

Stable

Fig. 13. Quality test for data subdivision in convective, adiabatic and stable conditions. (A)

Quality test for sensible heat. (B) Quality test for latent heat. (C) Quality test for carbon dioxide

flux.

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34

Energy balance closure

The turbulent fluxes of sensible and latent heat, net radiation, ground heat flux and energy

balance closure are calculated before and after the whole correction procedures. In Fig. 14A and

B, ensemble means of diurnal variations of turbulent fluxes over the whole experimental period

are shown. Correction procedures play an important role on all turbulent fluxes of latent and

sensible heat, and also ground heat has to be corrected for storage term to obtain a reliable flux

estimation. For ground heat flux the correction procedure (not described in this work) is required

to account for the heat storage that occurs in the layer between the soil surface and the heat flux

plate (Kustas and Daughtry, 1990). As shown in Fig.14A, if correction procedures are not

applied, during daytime, latent, sensible and ground heat fluxes collapsed to zero, while in

nighttime overestimations of latent and sensible heat leads to an unsatisfactory flux

interpretations. In Fig.14B, corrected fluxes have a typical trend described in literature, with

latent heat greater then sensible heat because the field is covered by the vegetation for a wide

range of the experimental period. In Fig. 14C, residual flux calculated as Rn-LE-H-G is shown.

Residual magnitude for uncorrected fluxes is characterized by peaks in daytime and nighttime,

with maximum values of about 400 W m-2

at 12 A.M and -300 W m-2

at 2 A.M.. Residual trend

for corrected fluxes is close to zero with the exception of some hours in the morning, where the

mean residual value is about 50 W m-2

.

A B

-100

0

100

200

300

400

500

600

0 3 6 9 12 15 18 21 24

Flu

xes

(W m

-2)

Hours

Rn

LE_uncorrected

H_uncorrected

G_uncorrected

-100

0

100

200

300

400

500

600

0 3 6 9 12 15 18 21 24

Flu

xes

(W m

-2)

Hours

Rn

LE_corrected

H_corrected

G_corrected

C

-300

0

300

600

0 3 6 9 12 15 18 21 24

Rn

-LE

-H-G

(W

m-2

)

Hours

Residual_uncorrected fluxes

Resudual_corrected fluxes

Fig. 14. Ensemble means of diurnal variation of turbulent (A, B) and residual (C) fluxes for the

whole period of the experimental campaign.

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35

The energy balance closure using all corrected fluxes (Fig. 15A) or only fluxes related to 0 and 1

quality classes (Fig. 15B), is shown. Even if the increase in energy balance closure is only of

about 4%, quality check permits to eliminate data which could be cause of major dispersion of

dots in respect 1:1 ideal line with R2 which comes from 0.75 to 0.80. Energy budget is typically

not closed when measuring energy fluxes with an eddy covariance station, available energy is

usually bigger than the sum of turbulent vertical heat fluxes with a ratio that varies between 70

and 98% (Jacobs et al., 2008; Meyers and Hollinger, 2004; Wilson et al., 2002; Foken et al.,

2006). As shown in Fig. 15A the slope of linear regression is 0.81 which is included in the range

of values which are usually described in literature. However, there are several aspects which

could give a relevant improvement in energy balance closure: the contribution of additional

storage fluxes such as photosynthesis flux, crop, air enthalpy changes (Jacobs at al., 2008;

Meyers and Hollinger, 2004), footprint shape and the representativeness of measured fluxes as a

function of scale (Shmid, 1997) to make mention of some problems. Usually for homogeneous

area it is considered valid the assumption that source areas are the same for all fluxes. However

these areas can be significantly different, if the footprint of turbulent fluxes is compared to the

source area of ground heat flux. So a portion of the error in energy balance closure can be related

to the difficulty to match footprint area of eddy covariance fluxes with the source areas of the net

radiation and heat flux plate instruments (Wilson et al., 2002).

A B

y = 0.81x

R² = 0.75

-200

0

200

400

600

800

-200 0 200 400 600 800 1000

LE

+H

(W

m-2

)

Rn-G (W m-2)

y = 0.85x

R² = 0.80

-200

0

200

400

600

800

-200 0 200 400 600 800 1000

LE

+H

(W

m-2

)

Rn-G (W m-2)

Fig. 15. Energy balance closure with all data set (A) and only with 0 and 1 quality fluxes (B).

Fluxes directly obtained from 30 minutes averaged data

As explained in Ueyama et al. (2012), in literature, it is unstill clear which data processing steps

are influential in the calculation of half-hourly and annual fluxes. According to results shown in

previous sections, WPL and VD corrections provide for a substantial fluxes modification,

influencing drastically cumulated evapotranspiration and carbon dioxide flux annual budgets.

These corrections are the heart of PEC software (Corbari et al., 2012), which is designed to

answer question of real time data management. With the objective to verify the possibility of

using eddy covariance station in an operative way for water irrigation management, so to

understand if averaged data at 30 minutes are still of good quality in respect to high frequency

data, the results obtained by PEC software are compared with those obtained by Eddy Pro 4.0.

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PEC software features

Data logger program has to be compiled to convert electrical signals, originated from sensors, in

physical measurements. Moreover, choosing an appropriated averaged interval, it can be set to

perform some elementary mathematical operations as mean, variance or covariance among

different measured variables. High frequency data will be lost but on the data logger memory

aggregated data which are at 30 minutes will be stored. Time step (averaged time) has been

chosen in accordance with results shown in different literature works as Lumley and Panofsky

(1964), Lenschow et al. (1994) and Gluhovsky and Agee (1994). According to these authors,

averaged time can not be less than 30-60 minutes if means, variances and covariance have to be

assessed with an accuracy of about 5-15%. The complete procedure implemented in PEC for real

time data management is reported in Corbari et al. (2012). Steps which describe the procedure

for turbulent fluxes calculation, can be summarized in four points:

1) Starting from averaged data, uncorrected fluxes (level 0) are calculated;

2) WPL and VD corrections are implemented;

3) Rainfall days are discarded;

4) Elimination of spikes is applied.

While points 1 and 2 are implemented with a programming language, points 3 and 4 are

performed manually by the operator. During rainfall periods the data are completely discarded

and if the rain falls during night time the data until the net radiation is greater than 0 W m-2

are

discarded. Despiking is applied on turbulent fluxes of latent, sensible heat and carbon dioxide in

accordance with the experience of the operator. Deep knowledge of site, cultivation typology and

literature data are the basic information which give to the operator the possibility to exclude, for

the analysis, turbulent fluxes which are not representative of the physical phenomena in the field.

In Tab. 2 the plausibility ranges for latent, sensible heat and carbon dioxide are shown.

Preliminary processes and spectral corrections have not been applied.

Tab. 2. Plausibility range for turbulent fluxes of latent, sensible heat and carbon dioxide

Min Max

Latent heat (W m-2

) -50 850

Sensible heat (W m-2

) -150 600

Carbon dioxide (millimol m-2

s-1

) -80 50

PEC fluxes in comparison with Eddy Pro 4.0 fluxes

In Fig. 16 two simple schemes which describe the levels of flux intensities applying the

sequences of correction procedures for Eddy Pro 4.0 and PEC software, are shown. Starting from

raw flux of latent heat (LE0), spectral correction factor is multiplied for LE0 obtaining LE1 and

subsequently WPL correction is added for the calculation of the definitive corrected flux LE3.

Using PEC software, LE3 is directly calculated applying only the WPL correction, and a flux loss

is shown as a consequence of spectral information losses. VD correction algorithm produces a

decrease of the raw flux of sensible heat from H0 to H2. Subsequently, it is multiplied for the

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37

spectral correction factor for sonic temperature, to obtain H3. Also in this case, using PEC

software, the data has not been opportunely corrected for spectral losses.

A B

In

ten

sit

y o

f la

ten

t h

ea

t (W

m-2

)

Eddy Pro 4.0 Averaged dataset

LE0

LE1

LE3

LE0

LE3Flux loss

In

ten

sit

y o

f sen

sib

le h

ea

t (W

m-2

) Eddy Pro 4.0 Averaged dataset

H0

H2

H3

H0

H3Flux loss

Fig. 16. Intensities of latent(A) and sensible(B) heat fluxes before and after the application of the

correction procedures using Eddy Pro 4.0 and PEC softwares.

The consequences of the spectral losses are remarked in the slope of linear regression between

PEC and Eddy Pro fluxes. Flux losses, for latent and sensible heat, produce a mean decrease in

flux magnitude of about 8%, with slopes equal to 0.95 for latent heat and 0.90 for sensible heat.

Intercepts are near closed to zero while R2 is about 0.9 for both fluxes.

Usually, engineering applications need to know evapotranspiration flux overall growing season.

Cumulated evapotranspiration flux and carbon dioxide trend could be used to define the

characteristics of canopy comportment from sowing to reaping time. In Fig.17, cumulated

evapotranspiration flux and carbon dioxide trend over growing season of maize field are shown.

In black, the fluxes calculated using Eddy Pro 4.0, and in grey the fluxes obtained by PEC

software are shown. As shown in Fig. 17A, the divergence among two fluxes starts at the

beginning of the growing season and it remains constant on all experimental period. As shown in

Fig. 17B, the divergence begins more or less at 200 Julian day and increases until the end of the

cultivated season. At the end of growing season the difference among the fluxes is about 10 mm

for the cumulated evapotranspiration and 90 g m-2

for CO2.

A B

0

50

100

150

200

250

300

140 160 180 200 220 240 260

Ev

ap

otr

an

spir

ati

on

(m

m)

Julian day

ET_from_averaged_data

ET_from_EddyPro

-1.2E+03

-9.0E+02

-6.0E+02

-3.0E+02

0.0E+00

3.0E+02

140 160 180 200 220 240 260

CO

2cu

mu

late

d f

lux

(g

m-2

)

Julian day

CO2_from_averaged_data

CO2_EddyPro

Fig. 17. Comparison between cumulated evapotranspiration (A) and carbon dioxide (B) fluxes

obtained by PEC and Eddy Pro 4.0 softwares.

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Energy balance closure with PEC fluxes

In order to complete the analysis over fluxes obtained by PEC software, energy balance closure

is shown in Fig. 18. The slope of the linear regression is quite differenced by that shown in Fig.

15A (obtained by Eddy Pro 4.0). In this case the slope is equal to 0.74, while the dispersion of

the dots is reduced and R2

value is about 0.89. This result is probably due to the moderated

influence of preliminary processes and spectral losses which have not been considered into the

PEC software corrections.

y = 0.74x

R² = 0.89

-200

0

200

400

600

800

-200 0 200 400 600 800

LE

+H

(W

m-2

)

Rn-G (W m-2)

Fig. 18. Energy balance closure using latent and sensible heat fluxes calculated by PEC software.

Conclusion

In this work the impact of different correction procedures on turbulent flux measurements

collected by an eddy covariance station, are described. Starting from high frequency data a

complex series of processes have to be implemented to extract reliable turbulent fluxes of latent,

sensible heat, carbon dioxide and water vapor from raw data measurements.

In the preliminary processes, the double correction procedure play a fundamental role to adjust

the orientation of the Cartesian system of axis respect to streamlines. Spectral corrections are

necessary to define flux losses due to the specific transfer functions which characterize the

measurement system. Turbulent fluxes need to be corrected for density fluctuation and humidity

effect on sonic temperature using WPL and VD corrections. These corrections should not be

considered as corrections, but a normal step to calculate turbulent fluxes. In fact, if the WPL and

VD corrections are not applied, turbulent fluxes do not reproduce correctly the physical aspects

of the experimental site. A final control based on micrometeorological tests of steady state and

developed turbulence permits to highlight the quality of calculated fluxes advising the operator if

flux data should be neglected.

High frequency (10-20 Hz) measurements of the three components of wind velocity and gas

concentrations have to be stored to obtain reliable turbulent fluxes at different scale. It is widely

known in literature, but in some cases, impossibility to have high frequency data do not permit to

apply the whole categories of correction procedures. Moreover, some engineering applications

which for example refer to the possibility to estimate evapotranspiration fluxes over a growing

season could not require for the accuracy developed in the previous analysis. For these problems,

a simple method which permits to the operator the possibility to calculate turbulent fluxes from

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39

an averaged dataset has been shown. In fact, in PEC software only WPL and VD corrections are

implemented and these corrections could be defined as essential ingredients to covert

measurements in reliable fluxes. As shown in Fig. 17A the difference between PEC software

results and Eddy Pro 4.0 fluxes is small and PEC fluxes underestimates Eddy Pro

evapotranspiration fluxes only for 10 mm. Reducing the number of corrections, the algorithm

implementations in a programming language appear to be of easy application also for operators

which are not expert in software engineering. In general it is possible to conclude that turbulent

fluxes could be approximately assessed starting from averaged data, but if the flux accuracies are

rigorously required, the whole range of corrections should be taken into account.

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(Chapter 2) – Energy balance closure of an eddy covariance station: limitations and improvements

Abstract

The use of energy fluxes data to validate land surface models requires that the conservation of

the energy balance closure is satisfied; but usually this condition is not verified when, measuring

energy components with an eddy covariance station, available energy is bigger than the sum of

turbulent vertical fluxes. In this work, a comprehensive evaluation of the energy balance closure

problems is performed on Livraga 2012 data set which is obtained by a micrometeorological

eddy covariance station located in a maize field in Po Valley. Energy balance closure is

calculated by statistical regression of turbulent energy fluxes and soil heat flux against available

energy. Generally, the results indicate a lack of closure with a mean imbalance in the order of

20%. Storage terms are the main reason for the unclosed energy balance but also the turbulent

mixing conditions play a fundamental role in the reliable turbulent flux estimations. Recently

introduced in literature, the energy balance problem has been studied as a scale problem.

Representative source area for each flux of the energy balance has been analyzed and the closure

has been performed in function of turbulent flux footprint areas. Surface heterogeneity and

seasonality effects have been studied with objective to understand the influence of canopy

growth on energy balance closure. High frequency data have been used to calculate co-spectral

and ogive functions which suggest if averaging period of 30 minutes may miss temporal scales

that contribute to the turbulent fluxes. Finally, latent and sensible heat random error estimations

are computed to give information about measurement system and turbulence transport

deficiencies.

Introduction

Surface energy fluxes are important for a huge range of application over different spatial and

temporal scales: from flash flood simulation at basin scale to water management in agricultural

area. It is then important to understand the quality of measured fluxes before using them for land

– atmosphere simulations.

The quality of eddy covariance measurements is influenced not only by possible deviations from

the theoretical assumptions but also by problems of sensor configurations and meteorological

conditions (Foken and Wichura, 1996). However, it is difficult to isolate the causes of

measurements errors. Instrumental errors, uncorrected sensor configurations, problem of

heterogeneities in the area and atmospheric conditions are the main problems that afflict the data

quality (Jacobs et al., 2008; Wilson et al., 2002; Foken et al., 2006; Foken, 2008a). Eddy

covariance method produces reliable results when the theoretical assumptions in the surface

layer are respected (Baldocchi et a. 2001; Foken and Wichura, 1996; Fisher et al., 2006). In

particular, the theoretical requirements, such as steady-state condition, horizontal homogeneity

of the field, validity of the mass conservation equation, negligible vertical density flux, turbulent

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fluxes constant with height and flat topography, should be satisfied. Moreover, sensors

configuration should be analyzed in relation to the sampling duration and frequency, separation

of sonic anemometer and gas analyzer, sensor placement within the constant flux layer, but out

of the roughness sub-layer. Meteorological conditions, such as precipitation events and low

turbulence, especially at night time, can lead to errors in fluxes measurement.

The unbalance of the energy budget has been widely studied in the last decade due to the fact

that the use of energy fluxes to validate land surface models requires that the closure of the

energy balance is satisfied. Energy budget is typically not closed when, measuring energy fluxes

with an eddy covariance station, available energy is usually bigger than the sum of turbulent

vertical heat fluxes with a ratio that varies between 70 and 90% (Jacobs et al., 2008; Wilson et

al., 2002; Foken et al., 2006; Ma et al., 2009). Thus, it is important to understand the different

factors that can lead to an improvement of the energy balance closure.

The first cause of the lack of energy balance closure is liked to an uncorrected implementation of

a complete set of instrumental and flux corrections as described in Aubinet et al. (2000). Axis

rotation, spike removal, time lag compensation and detrending are the preliminary correction

processes which should be applied on high frequency raw data set measured by sonic

anemometer and gas analyzer. Subsequently, spectral information losses, air density fluctuations

and humidity effects have to be taken into account to obtain reliable fluxes of latent and sensible

heat (Moncrieff et al. 1997,Webb et al. 1980; Van Dijk et al. 2004).

However, later studies discuss unbalance problem as an effect of the fractional coverage of

vegetation and the influence of the soil storage (Foken, 2008b). Additional storage terms, like the

ones linked to the photosynthesis processes or vegetation canopy, give a relevant improvement

in energy balance closure (Meyers and Hollinger, 2004).

Different time aggregation could reduce the effect of storage terms because they have an

opposite behavior during day time and night time (Papale et al., 2006). Some recent works

(Finnigan et al., 2003; Oncley et al., 1993) have suggested that averaged time (generally 30

minutes) which is chosen to calculate covariances could be inadequate for assessing turbulent

fluxes. Ogive function for each half hour data set can be a good indicator for measurement errors

associated to such energy balance problems (Oncley et al., 1993).

Moreover, energy balance closure can be seen as a scale problem, because the representativeness

of a measured flux is a function of scale. Usually, for homogeneous areas, the assumption that

source areas are the same for all fluxes is considered valid. However, these areas can be

significantly different if the footprint of turbulent fluxes is compared to the source area of ground

heat flux. So a portion of the error in energy balance closure can be related to the difficulty to

match footprint area of eddy covariance fluxes with the source areas of the instruments which

measure net radiation and ground heat flux (Wilson et al., 2002; Schmid, 1997; Hsieh et al

2000).

Eddy flux measurements can be underestimated during periods with low turbulence and air

mixing. This underestimation acts as a selective systematic error and it generally occurs during

the night time. Massman and Lee (2002) listed the possible causes of the night-time flux error.

There is now a large consensus to recognize that the most probable cause of error is the presence

of small scale movements associated with drainage flows or land breezes that take place in low

turbulence conditions and create a decoupling between the soil surface and the canopy top. In

these conditions, advection becomes an important term in the flux balance and cannot be

neglected anymore. It has been recently suggested (Finnigan et al., 2006) that, contrary to what

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45

was thought before, advection probably affects most of the sites, including also flat and

homogeneous ones. Direct advection fluxes measurements are difficult to measure as they

require several measurement towers at the same site. Attempts are notably made by Aubinet et

al. (2003), Feigenwinter et al. (2004), Staebler and Fitzjarrald (2004) and Marcolla et al. (2005).

They find that advection fluxes are usually significant during calm weather conditions. However,

in most cases, the measurement uncertainty is too large to allow their precise estimation. In

addition, such direct measurements require a too complicated set up to allow routine

measurements at each site. In practice, flux problem is by-passed by discarding the data

corresponding to low mixed periods. The friction velocity is currently used as a criterion to

discriminate low and high mixed periods. This approach is generally known as the “u∗

correction”. Although being currently the best and most widely used method to circumvent the

problem, the u∗ correction is affected by several drawbacks and must be applied with care.

Factors connected with growing vegetation and seasonality have been investigated. As shown in

Panin et al. (1998) the unbalance could be attributed to the influence of the surface heterogeneity

and vegetation height in respect to sensors position.

Different sources of uncertainties in flux measurements can be sometimes difficult to assess.

Random measurement errors in flux data, including errors due to measurement system and

turbulence transport, have been assessed by Hollinger and Richardson (2005), comparing the

measurements from two towers with the same flux source area (“footprint”) and by Richardson

et al. (2006), comparing pair of measurements made on two successive days from the same tower

under equivalent environmental conditions. A simple method described in Moncrieff et al.

(1996) can be used to quantify the influence of random error on momentum, latent and sensible

heat calculating a degree of uncertainty for each turbulent flux.

In this work relevant findings on energy balance closure problem over maize field in Po Valley

are summarized mainly on the basis of recent investigation works as Foken (2008b), Oncley et

al. (2007) and Wilson et al. (2002). Turbulent fluxes from a raw data set of high frequency

measurements, are obtained using Eddy Pro 4.0 software with the main objective to standardize

the correction procedure of eddy covariance measurements. Impacts of each investigated factor

is quantified by the slope and intercept values between turbulent vertical heat fluxes (latent heat,

sensible heat and ground heat fluxes) and available energy (net radiation) from a regression

analysis of half hourly basis. Each examined factor is separately studied to each other to improve

understanding of its impact on energy balance closure. Theoretical backgrounds are not

summarized in a separate chapter but they are included in each sub-paragraph to improve the

description of the exanimate problems. Only practical formulas are shown, while mathematical

approaches are quoted in literature.

Instruments, data collection and site description

Experimental campaign was carried out over a maize field at Livraga (LO) in Po Valley during

the year 2012. The field is about 10 hectare large and the local overall topography is flat. In the

middle of the field an island of about 50 m2 is designed to include agro-micrometeorological

instruments and devices.

Eddy covariance data are measured by a tridimensional sonic anemometer (Young 81000) and

open path gas analyzer (LICOR 7500) located at the top of a tower at an height of about 5 m.

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46

High frequency (20 Hz) measurements are stored in a compact flesh of 2 Gb connected with the

data logger Campbell CR5000 and downloaded in situ weekly. On compact flash only three wind

velocity components, sonic temperature, vapor and carbon dioxide concentrations are stored (raw

data). Contemporaneously net radiation, measured by CNR1 Kipp&Zonen radiometer (4.5 m

high), soil heat flux, measured by HFP01 Campbell Scientific flux plate, and soil temperature

measurements are stored on data logger in different memory tables. Into the island also soil

moisture at different levels and rain are measured. Averaged fluxes are calculated over a time

step of 30 minutes.

Experimental measurements were carried out from 21 May to 7 September but the dataset is

composed by only 3103 averaged data because some gaps due to malfunctioning of

instrumentations or rainfall days are shown into the data sequences. From 131 to 241 Julian day

the field is covered by vegetation, while the remaining days of the year, the field is characterized

by bare soil. Vegetation height varies from zero to 320 cm and the canopy grew during the

project can be spatially considered homogeneous across the field.

Wind direction is quite steady, generally from West during day time and East during night time

but in some days this convention is not always respected. Considering each wind direction, the

eddy tower position is compatible with the constant flux layer (CFL) (Elliot, 1958). CFL is

defined as 10-15% of internal boundary layer (Baldocchi and Rao, 1995), and it represents a

space area where measured fluxes by the eddy tower are constant. Applying Elliot’s (1958)

formula in unfavourable conditions of bare soil, with a calculated aerodynamic roughness of

about 0.04 m (Garrat, 1993), the CFL depth at the tower is about 6 meters ensuring that the eddy

covariance instruments (tridimentional sonic anemometer and gas analyser) are included into the

CFL.

During the summer period the site is typically characterized by a cloud-free sky in association

with a quit high evapotranspiration and net radiation values of about 600 and 700 W m-2

respectively. Cumulated rain over the experimental period is about 200 mm, while soil moisture

measured at a depth of 10 cm varies between maximum and minimum peaks of about 0.4 and

0.15 respectively.

The energy balance closure problem

Energy balance closure, a formulation of the first law of thermodynamic, requires that the sum of

the estimated latent (LE) and sensible (H) heat and ground heat flux (G) has to be equivalent to

all other energy sink or source (Eq. 1).

nRGHLE (1)

Where Rn is the net radiation. Generally, fluxes are typically integrated over periods of half hour

building the basis to calculate energy balance to annual time scales. The slope (defined as

(LE+H+G)Rn-1

) and intercept values of the regression line quantify the reliability of the energy

balance closure which is close to 1 in an ideal case. In the following sections the relevant

findings on the energy balance closure are summarized and data processing results using the

experimental measurements are shown.

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47

Effect of data corrections

In this paragraph the procedures necessary to obtain reliable fluxes starting from high frequency

raw data set are briefly described (see Chapter 1).

Eddy covariance measurements have to be corrected to obtain reliable turbulent fluxes of latent

and sensible heat. Before calculating fluxes, two groups of corrections should be implemented:

“instrumental” and “physical” corrections.

Instrumental corrections can be considered as preliminary processes which have to be directly

applied on high frequency measurements to prepare the data set for fluxes calculation.

Axis rotation for tilt correction. Tilt correction algorithms are necessary to correct wind statistics

for any misalignment of the sonic anemometer with respect to the local wind streamlines.

Wilczak et al. (2001), proposes three typologies of correction algorithms, and for Livraga 2012

dataset a double rotation method has been used. Using this method, the anemometer tilt is

compensated by rotating raw wind components to nullify the average cross-stream and vertical

wind components.

Spike removal. The so called despiking procedure consists in detecting and eliminating short

term outranged values in the time series. Following Vickers and Mahrt (1997), for each variable

a spike is detected as up to three consecutive outliers with respect to a plausibility range defined

within a certain time window, which moves throughout the time series.

Time lag compensation. In open path system the time lag between anemometric variables and

variables measured by gas analyzer is due to the physical distance between the two instruments,

which are usually placed several decimeters or less apart to avoid mutual disturbances. The wind

field takes some time to travel from one instrument to the other, resulting in a certain delay

between the moments the same air parcel is sampled by the two instruments (Runkle et al.,

2012).

Detrending. Eddy correlation method of calculating fluxes requires that the fluctuating

components of the measured signals are derived by subtracting them from the mean signals. In

steady-state conditions simple linear means would be adequate, but steady state conditions rarely

exist in the atmosphere and it is necessary to remove the long term trends in the data which do

not contribute to the flux (Gash and Culf, 1996).

After completing the preliminary processes, physical corrections have to be implemented.

Spectral information losses, air density fluctuation and humidity effects on sonic temperature are

taken into account in accordance with the procedure described in Ueyama et al. (2012).

Spectral correction. Spectral corrections compensate flux underestimations due to two distinct

effects. The first is referred to the fluxes which are calculated on a finite averaging time,

implying that longer-term turbulent contributions are under-sampled at some extent, or

completely. The correction for these flux losses is referred to as high-pass filtering correction

because the detrending method acts similarly to a high-pass filter, by attenuating flux

contributions in the frequency range close to the flux averaging interval. The second is connected

with instrument and setup limitations that do not allow sampling the full spatiotemporal

turbulence fluctuations and necessarily imply some space or time averaging of smaller eddies, as

well as actual dampening of the small-scale turbulent fluctuations (Moncrieff et al., 1997).

WPL correction. The open-path gas analyzer does not measure nondimensional carbon dioxide

and water vapor concentrations as mixing ratios but it measures carbon dioxide and water vapor

densities. For this reason, the trace gas flux using this analyzer needs to correct for the mean

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48

vertical flow due to air density fluctuation. Webb et al. (1980) suggested that the flux due to the

mean vertical flow cannot be neglected for trace gases such as water vapor and carbon dioxide.

To evaluate the magnitude of the influence by the mean vertical flow, Webb et al. (1980)

assumed that the vertical flux of dry air should be zero. Practically, sensible and latent heat

fluxes evaluated by the eddy covariance technique are used to calculate water vapor and carbon

dioxide fluxes by the mean vertical flow (WPL correction).

VD correction. Sonic anemometer measures wind velocity components and sonic temperature.

Sonic temperature, which is the basis of the sensible heat calculation, is affected by both

humidity and velocity fluctuations. Van Dijk et al. (2004), revising the experiment carried out by

Schotanus et al. (1983), defines a correction term to apply on sensible heat formula to obtain

reliable flux (VD correction).

Corrections impact on turbulent fluxes as a consequence of the procedure described above, can

be founded in the work of Ueyama et al. (2012) and also in Chapter 1 of this thesis. As shown in

Chapter 1, where ensemble means of diurnal variations of turbulent fluxes over the whole

experimental period are computed, if correction procedures are not applied, during daytime,

latent, sensible and ground heat fluxes collapsed to zero, while in nighttime overestimations of

latent and sensible heat brings to an unsatisfactory flux interpretations.

The energy balance closure calculated after the correction procedures only applied on latent and

sensible heat flux components is equal to 0.75 with a correlation coefficient (R2) of about 0.8 and

intercept of about 10 W m-2

.

Effect of storage terms

Eddy covariance measurements are based on turbulent air mixing and vertical flux exchanges.

Sometimes, portion of latent and sensible heat could be stored below measurement point and

these concentrations are not measured by anemometer and gas analyzer devices. Usually, when

the canopy covers the field, the effect of the canopy heat storage and photosynthesis flux

increase drastically. The best way to compute storage flux is to deduce it from a concentration

profile method inside the canopy (Papale et al, 2006). However, at many sites, a discrete

estimation based only on concentration at the tower top is used (Meyer and Hollinger, 2004).

Moreover, a correction is required to account for the heat storage that occurs in the layer between

the soil surface and the heat flux plate (Mayocchi and Bristow, 1995), so Eq. 1 can be rewritten

adding the storage terms (Eq. 2).

npcg RSSSGHLE (2)

Where Sp is the energy flux for photosynthesis, Sc is the canopy heat storage in biomass and

water content and Sg is the ground heat storage above the soil heat plate.

The heat storage terms for the local surface energy balance are calculated by computing the total

enthalpy change over a given time interval ( t ) which is 30 minutes. For the canopy, the rate

change in enthalpy is described by Eq.3.

t

cmcmS bbww

c (3)

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49

Where is the temperature exchange over the canopy directly measured by radiometer. In

fact, CNR1 Kipp & Zonen radiometer permits to measure directly long wave and short wave

radiation incoming and outgoing the surface. Starting from long wave radiation outgoing the

surface, considering the surface as a bleakbody, temperature can be calculated inverting Stefan-

Boltzmann law. Plant water mass (mw), biomass (mb) density, specific heat for plant water (cw)

and biomass (cb) are directly estimated by Meyers and Hollinger (2004) work, where the maize

plant were weighed, dried, and weighed again in order to assess the plant water content and

biomass density.

A similar procedure for heat storage in the soil surface is followed (Eq. 4).

t

zcmcTS ssswww

g (4)

Where T is the temperature exchange in the soil, msw is the density of water, w

is the measured

volumetric content measured by soil moisture probe at 10 cm depth, z is the depth above the

soil heat plate to the ground surface, sis the soil bulk density and cs is the specific heat capacity

of soil (Kustas and Daughtry, 1990).

The light energy transformed in the photosynthetic process to carbon bond energy in biomass has

long been ignored when compared to the other terms in the surface energy balance. However, as

researchers continue to be plagued by a lack of closure in the surface energy balance (Meyer and

Hollinger, 2004) all of the data processing methods and terms should be reevaluated.

Analyzing the formation of glucose in its chemical reaction (Eq.5), an estimate of the energy

used in photosynthesis is obtained from the net sum of the energy that is required to break the

bonds of the reactants and those in forming glucose and oxygen.

6H2O + 6CO2 ⇒ 6O2 + C6H12O6 (5)

This is the solar energy that is now stored in the bonds of carbohydrate and is ≈422 kJ of energy

per mole of CO2 fixed by photosynthesis (Nobel, 1974). A canopy assimilation rate of 2.5 mg

CO2 m−2

s−1

equates to an energy flux of 28 W m−2

. This conversion factor is used to compute the

measured photosynthesis rates from the eddy covariance measurements to an equivalent energy

flux.

In accordance with Meyers and Hollinger (2004) procedure, storage terms are computed for the

daytime period only and the data are grouped into 2 hours bins beginning at 6:00 and ending to

18:00. The averaged daytime storage fluxes for the whole experimental period are shown in Fig.

1. As shown in Fig.1A, heat storage in the soil is grater then the other storage fluxes. Its trend is

characterized by a peak of about 34 W m-2

in correspondence with the midday. During the

morning, heat storage in the soil increases while in the afternoon it decreases up to 10 W m-2

.

Photosynthesis storage term have a similar behavior with a peak of about 10 W m-2

, while the

canopy heat storage term tend to decrease during the day. In Fig. 1B the ratio between the sum of

storage terms (Total storage) and net radiation, which represents the available energy in the

ecosystem, is shown. The storage fluxes constitute a significant fraction of the available energy

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50

with a ratio of about 10% which is quite constant from 8:00 to 14:00, while it tends to decrease

in the late afternoon.

A B

-10

0

10

20

30

40

6-8 8-10 10-12 12-14 14-16 16-18

En

erg

y f

lux

( W

m-2

)

Hours

Sc

Sp

Sg

-5

0

5

10

15

6-8 8-10 10-12 12-14 14-16 16-18

To

tal st

ora

ge/

Rn

(%)

Hours

Fig. 1. A. The average daytime cycle for each storage term for the whole experimental perid. B.

Fraction of net radiation that is portioned to storage for maize plants.

The effect of storage terms on surface energy balance is examined by comparing the sum of H,

LE and G with and without each storage flux against Rn for the daytime periods over the whole

experimental campaign. For the maize filed, without including the storage terms, the slope from

simple linear regression is 0.75 with an R2 of about 0.8 (Fig. 2). When the storage terms, in the

surface energy balance, are included the slope of the linear regression tends to increase up to

0.86 with a R2

of about 0.8 and an intercept of about 1.8 W m-2

. If in the energy balance closure

storage terms are included, the systematic error in fluxes, described by linear regression

intercept, is characterized by a drastic decreasing from 10 W m-2

to 1.8 W m-2

. As explained in

Foken (2008a), the ground heat storage has to be added into soil heat flux to obtain reliable G

flux estimation. In fact, as shown in Fig. 2, ground storage term plays a fundament role into the

energy balance closure improvement having a positive influence of about 6% which is equal to

about 54% over the total energy balance improvement if the whole storage terms are considered.

0

4

8

12

0.68

0.72

0.76

0.8

0.84

0.88

Inte

rcep

t (

W m

-2)

Slo

pe

an

d R

2(-

)

Slope

R2

Intercept

Fig. 2. Energy balance closure adding storage terms.

Although the daytime energy balance with total storage terms is on average closed within 14%,

closure deficit may be a consequence of an inaccurate G flux estimation which is extremely

different in the spatial contest as described in Wilson et al. (2002). Moreover, storage fluxes

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51

obtained by a single point measurement can be underestimated in respect to the more

complicated profile methods.

In the common practice, heat soil flux (measured by heat soil plate) is usually corrected with

ground storage term, so that, in the following paragraphs, in G flux the ground heat storage term

is already included.

Effect of time aggregation

As described in Foken (2008b), an energy transport with large eddies which cannot be measured

with the eddy covariance method is assumed as one of the main reasons of the closure problems.

In literature, several methods are discussed to investigate this problem (Sakai et al. 2001,

Finnigan et al. 2003, Foken et al. 2006). About 15 years ago, the ogive function was introduced

into the investigation of turbulent fluxes (Oncley et al. 1990, Friehe 1991). This function was

proposed as a test to check if all low frequency parts are included in the turbulent flux measured

with the eddy covariance method (Foken et al. 1995). The ogive function is the cumulative

integral of the co-spectrum starting with the highest frequencies as described by Eq.6.

0

)()( 0

f

wxwx dffCofOg (6)

where Cowx is the co-spectrum of a turbulent flux, w is the vertical wind component, x is the

horizontal wind component or scalar, and f is the frequency. In Fig. 3 sensible and latent heat

flux cospectrums and their ogive functions are respectively shown. In Fig. 3A example of a

ogive function and co-spectrum for ''Tw in 20 July at 14:00 is shown, while in Fig. 3B example

of a ogive function and co-spectrum for '' 2OHw in 11 August at 03:30 is shown.

A B

-2

0

2

4

6

0.00010.0010.010.1110

0

30

60

90

120

0.00010.0010.010.1110

Co

WT

Og

WT

Frequency (Hz)

Ogive (WT)

Cospectrum (WT)

-20

-10

0

10

20

30

40

0.00010.00100.01000.10001.000010.0000

-30

0

30

60

90

120

150

0.00010.00100.01000.10001.000010.0000

Co

WH

2O

Og

WH

2O

Frequency (Hz)

Ogive (WH2O)

Cospectrum (WH2O)

Fig. 3. Example of a ogive function and cospectrum for ''Tw (A) and '' 2OHw (B) in 20 July at

14:00 and 11 August at 03:30 respectively.

In the convergent case (Fig.3A), the ogive function increases during the integration from high

frequencies to low frequencies until a certain value is reached and remains on a more or less

constant plateau before a 30 minutes integration time. If this condition is full-filled, the 30

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52

minutes covariance is a reliable estimate for the turbulent flux, because it is possible to assume

that the whole turbulent spectrum is covered within that interval and that there are only

negligible flux contributions from longer wavelengths (Case 1). But it can also occur that the

ogive function shows an extreme value and decreases again afterwards (Case 2- Fig.3B) or that

the ogive function doesn’t show a plateau but increases throughout (Case 3). Ogive functions

corresponding to Case 2 or 3 indicate that a 30 minutes flux estimate is possibly inadequate.

Foken et al. (2006) define thresholds about ogive characteristic behaviors in order to prescribe if

a ogive belongs to Case 1, 2 or 3.

From the ogive analysis performed for latent and sensible heat fluxes over the whole

experimental period, 30 minutes averaging interval appears to be sufficient to cover all relevant

flux contributions with about 80% of cases included in the Case 1, while only 20% of cases

belongs to Case 2 and 3.

Finnigam et al. (2003) propose a site specific extension of the averaging time up to several hours

to close the energy balance. In Fig. 4 energy balance closures with reference to energy flux

aggregations at different temporal scales, are shown.

-50

-30

-10

10

30

0.7

0.75

0.8

0.85

0.9

0.95

0.5 hour 6 hour 24 hour

Inte

rcep

t (W

m-2

)

Slo

pe

an

d R

2(-

)

Slope

R2

Intercept

Fig. 4. Energy balance closure with different aggregation times.

The slope tends to increase if large size of averaging time are considered, but if an aggregation

period of 6 hours is examined, the linear regression (0.76) is quite similar to that calculated with

half-hourly data (0.75). Instead, with an aggregation time period equal to 24 hours, the slope has

a large improvement (0.83). This is probably due to the effect of storage terms which can be

considered negligible at daily scale as shown in Foken (2008b).

Effect of scale differences in fluxes measurement

The energy balance closure can also be seen as a scale problem, because each flux is

representative of an area (Fig.5). In fact net radiometer source area is the field of view of the

instrument at nadir related to sensor height and it doesn’t change with time. In Fig.5A the net

radiometer source area described by Schmid’s (1997) equation using the radiometer

configuration on the tower for this experimental campaign, is shown. Radiometer is located on a

arm (b) of about 2.5m long, attached on the tower at the height of about 4.5 m (zr). Its orientation

is from North to South to receive the whole solar radiation during the daily hours. Its source area

has a circular shape with a maximum radius of about 4 m, and the major representativeness of

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53

the short and long wave measurement, which are coming from the surface, are in correspondence

with the projection of the radiometer on the ground (red zones).

The flux footprint of turbulent fluxes varies in space and time depending mainly on wind

velocity and direction, surface roughness, stability condition of the atmosphere and measurement

height (Hsieh et al., 2000). According to Hsieh et al. (2000) definition, the footprint represents a

weight function (for unit of length) of different contribution that is coming from the surface area

at a certain distance away for the instruments (anemometer and gas analyzer - EC station). This

function change in space and in time and it is different for each 30 minutes measurement. In Fig.

5B footprint source area of the eddy covariance station considering the whole experimental data

from May to September, is shown. Bi-dimensional footprint is computed using Hsieh et al.

(2000) and Detto et al. (2006) models for the longitudinal and lateral spreads respectively. The

mathematical approach to match Hsieh et al. (2000) and Detto et al. (2006) models is not

described in this work but it is widely discussed in the recent article of van de Boer et al. (2013).

The footprint area obtained for each half-hourly data has been oriented in respect to the wind

directions, and performing this procedure on the whole experimental data set, the footprint shape

represented in Fig. 5B has been obtained. In general, the major representativeness of the latent

and sensible heat flux measurements is confined in an area of about 450m2 on the right of the

tower (West direction). This is probably due to the limited magnitude of the wind intensities in

Po Valley which are not exceeded 10 m s-1

.

A B

zr

b

projection of the

radiometer center

Radiometer

footprint (m-2)

zm

EC station

EC station

footprint (m-1)

zm

Fig. 5. A. Radiometer source area. B. Footprint source area for eddy covariance instruments. (b)

arm length , (zr) radiometer height, (EC station) eddy covariance instruments (gas analyzer and

sonic anemometer), (zm) eddy covariance instrument heights.

The effect of flux spatial scales on energy balance closure is evaluated considering the peak

location of the footprint function inside the field. As shown in Fig. 6, the peak data have been

subdivided into four percentile groups (each with 25% of the data) so that turbulent fluxes of

latent and sensible heat connected to each peak are used to compute the energy balance closure.

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54

0

2

4

6

8

10

12

0.4

0.6

0.8

1.0

6 - 25% 10- 50% 22 - 75% 628 - 100%

Inte

rcep

t (

W m

-2)

Slo

pe

an

d R

2(-

)

xpeak (m) - percentile

Slope

R2

Intercept

Fig. 6. Energy balance closure for four 25 percentile groups of footprint function peak location

(xpeak).

The energy balance closure tends to increase when the peak location is far from the eddy

covariance station up to 22 m. The maximum value of the linear regression slope is 0.88 in

correspondence with 75 percentile group, i.e. with the footprint peak far from the tower which

varies between 10 and 22 meters. However, when the peak exceeds 22 m the slope tends to

decrease probably because representative source area of eddy covariance measurements exceed

the field dimension. Instead, when the peak location is near the station the heterogeneity of the

island surface (which is sown by hand) and devices influence could create alteration in turbulent

flux measurements. The systematic error defined by intercept, increases linearly with the

percentile groups up to 9.7 W m-2

.

Ground heat flux is usually very small in respect to the other energy fluxes, ranging from 5 to 40

% of net radiation but this flux is the one with the highest uncertainty in its estimate that can

reach an error up to 50% (Foken, 2008a). Moreover, it is measured with an instrument with the

smallest source area that can be up to two orders of magnitude lower than latent and sensible

heat fluxes footprints. So that it can be very changeable in a field due to different soil

characteristics or soil moisture conditions as shown in Kustas et al. (2000), where they found

that, measuring G with 20 instruments in a small site, mean differences in soil heat flux are of

about 40 W m-2

but they can deviate in some occasion also of 100 Wm-2

. Investigation of

variation of heat soil flux across the field and its influences on energy balance closure, is an

important issue which has been studied by many scientists. In the current state, G is assumed

uniform on the field and its strong variability across the field is in first approximation neglected.

Effect of turbulent mixing

The effect of turbulent mixing is evaluated in respect to friction velocity (u*). Friction velocity

typically changes with stability of atmosphere and time of day as explained in Wilson et al.

(2002). The change in energy balance closure could also be the direct result of changes in

friction velocity. In accordance with Wilson et al. (2002), a simple method used to isolate the

effects of friction velocity on energy balance improvement, is shown. Data are separated into

four 25 percentile groups, and each group contains data when the friction velocity is included

among two consecutive friction velocity percentile values. Slope of the linear regression, R2 and

intercept are also evaluated during daytime and night time as shown in Fig.7. As explained in

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55

Fig. 7A, during daytime the slope increases from 0.73 to 0.85 and the intercept varies from -1 to

2 W m-2

. Only when friction velocity is included between 0.28 and 0.83 m s-1

, intercept

collapsed on a value of about 0.7 W m-2

. During nighttime (Fig. 7B) energy balance closure is

drastically worsen with a mean slope of about 0.06. Intercept is quite closed to 0 W m-2

while R2

considerably varies among the percentile groups. This is probably due to low wind velocities

which, during nighttime, prevent the well turbulent mixed conditions of the atmosphere

increasing the advection transport of scalar fluxes and worsening the eddy covariance

measurements.

A B

-2

0

2

4

6

0.4

0.6

0.8

1.0

0.14-25% 0.21-50% 0.28-75% 0.83-100%

Inte

rcep

t (W

m-2

)

Slo

pe

an

d R

2(-

)

u* (m s-1) - percentile

Slope

R2

Intercept

-6

-4

-2

0

2

4

6

0.00

0.02

0.04

0.06

0.08

0.10

0.12

0.06-25% 0.09-50% 0.15-75% 0.69-100%

Inte

rcep

t (W

m-2

)

Slo

pe

an

d R

2(-

)

u* (m s-1) - percentile

Slope

R2

Intercept

Fig. 7. Energy balance closure for four 25 percentile groups of u* friction velocities. A. Daytime.

B. Nighttime.

In Fig. 8, friction velocity influence on energy balance closure globally evaluated for the whole

experimental data set, is shown. The slope constantly increases up to 0.82 when the data are

included in a friction velocity range between 0.24 and 0.83 m s-1

. The systematic errors defined

by the intercept values tend to decrease, and in correspondence with a closure of 0.82 the

intercept value is about 4.3 W m-2

. Literature results (Wilson et al., 2002; Barr et al., 2006) are

also confirmed from the analysis performed at Livraga station, given that with the increase of

friction velocity the closure of the energy budget tends to increase as well. In fact when the

friction velocity is low, the turbulence is softened and the fluxes are usually underestimated. The

problem related to the use of friction velocity as an indicator of good measured data is linked to a

u* threshold definition. In Alavi et al. (2006) a value of 0.1 m s-1

is considered, while Oliphant et

al. (2004) use 0.3 m s-1

and Barr et al. (2006) 0.35 m s-1

, showing that the choice of this limit on

u* seems to be site dependent.

0

2

4

6

8

10

0

0.2

0.4

0.6

0.8

1

0.08 - 25% 0.15 - 50% 0.24 - 75% 0.83 - 100%

Inte

rcep

t (W

m-2

)

Slo

pe

an

d R

2(-

)

u* (m s-1) - percentile

Slope

R2

Intercept

Fig. 8. Energy balance closure for four 25 percentile groups of u* friction velocities for the

whole experimental dataset.

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56

Effect of vegetation

Many experimental results about energy balance problems above low and tall vegetations are

available in literature (Wilson et al., 2002; Aubinet et al., 2000; Panin et al., 1998). Here, the

influence of the vegetation height and heterogeneity on energy balance closure is studied

subdividing the experimental data set into five classes from C1 to C5. Each class contains data

with different vegetation height (Tab. 1) in function of canopy growth.

Tab. 1. Vegetation height classis.

Class Vegetation height (cm)

C1 From 0 to 30

C2 From 30 to 60

C3 From 60 to 90

C4 From 90 to 150

C5 From 150 to 320

For each class the energy balance closure is calculated and the results are shown in Fig. 9A. The

slope tends to decrease, with an increase of vegetation height, up to 0.76 for a canopy height

between 150 and 320 cm. The maximum slope value is about 0.98 in correspondence with C1

class when the surface heterogeneity is particularly accentuated. Intercept changes its plus sign

in correspondence with C5 class, where the intercept value is about -3.4 W m-2

. To better

understand how these results are possible, the storage terms should be taken into account. In Fig.

9B, the slopes of the linear regression is compared with the percentage storage weights defined

by Eq.7. Storage weight is the ratio between the averaged storage fluxes for each class and the

sum of these averages on the whole class subdivisions.

1001

1

5

1 1

1

j j

N

i

i

N

i

i

x

SxN

SxN

weightStorage (7)

Where S is the storage term for the x flux (soil heat ground, photosynthesis or canopy storages),

N is the number of data for each class and j is a class indicator so that when it is equal to 1 it

represents C1 class, when it is equal to 2 it represents C2 class, and so on.

As shown in Fig. 9B, the slope trend is opposite to canopy and photosynthesis storage weight

terms. In fact, when the canopy is tall the weights of Sc and Sp are particularly relevant reaching

the value of about 35% in correspondence with C5 class. Instead, the soil heat ground storage

weight term drastically decreases when the vegetation is tall, moving it from 25% to 5% when

the class changes from C4 to C5. The presence of vegetation which covers the field play a

fundamental role in energy balance closure. In particular way, during the canopy growth, the Sp

and Sc storage terms increase their influence on energy balance closure and if they are not

considered the energy unbalance is accentuated. When the vegetation is lowed Sp and Sc effects

can be neglected while Sg becomes relevant reaching the weight value of about 30% (C1 class).

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57

A B

-4

-3

-2

-1

0

1

0.7

0.8

0.9

1

1.1

C1 C2 C3 C4 C5

Inte

rcep

t (W

m-2

)

Slo

pe

an

d R

2(-

)

Slope

R2

Intercept

0

10

20

30

40

50

60

0.6

0.7

0.8

0.9

1

1.1

C1 C2 C3 C4 C5

Sto

rag

e w

eig

ht

(%)

Slo

pe

(-)

Slope

Sg

Sc

Sp

Fig. 9. A. Energy balance closure for five class of vegetation height. B. Slope and storage weight

terms in function of vegetation height classes.

Effect of seasonality

To clearly describe the partition of energy balance components during different seasons, the

daily patterns of the 30 minutes averages of Rn, LE, H and G in May, June, July and August are

plotted in Fig.10. Net radiation maximum peak is quite constant from May to August oscillating

between 500 and 600 W m-2

. Latent and sensible heat have a strong variability trough the

months, showing a quite similar trend from May to June while in July and August latent heat is

about 3 times greater than sensible heat. The soil heat flux accounts for a small proportion of the

available energy, in particular way, when the vegetation covers the field surface. In fact, in May

at 12:00 it can also reach the maximum value of about 100 W m-2

, while in July and August the

soil heat flux is equal to few tens of watt to meter square.

The partitioning of net radiation into sensible heat and latent heat fluxes is strongly influenced by

change in vegetative characteristics. Specifically, when the vegetation is tall, the dominant

component of the energy budget is represented by latent heat with a peak in July of about 450 W

m-2

. Sensible heat is the main energy component when the vegetation is absented. It tends to

decrease during the canopy growth but, as shown in August, when the vegetation is fully

developed, it returns to be similar to values shown in May. One special phenomenon, called the

“oasis effect” can be noted in July when latent heat is the main component which takes the

largest portion of Rn and sensible heat is very small. In the case of optimum conditions for

evaporation, i.e. high soil moisture and well turbulent conditions (Foken, 2008a), the evaporation

process will be greater than the sensible heat flux. In such cases, sensible heat changes its sign 1-

3 hours before sunset and sometimes in the shortly afternoon, occurring in the atmosphere a

temperature gradient inversion and a downwarded sensible heat transfer.

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58

A B

-100

0

100

200

300

400

500

600

0 3 6 9 12 15 18 21 24

Flu

xes

( W

m-2

)

Hours

Rn

LE

H

G

-100

0

100

200

300

400

500

600

0 3 6 9 12 15 18 21 24

Flu

xes

( W

m-2

)

Hours

Rn

LE

H

G

C D

-100

0

100

200

300

400

500

600

700

0 3 6 9 12 15 18 21 24

Flu

xes

( W

m-2

)

Hours

Rn

LE

H

G

-100

0

100

200

300

400

500

600

0 3 6 9 12 15 18 21 24

Flu

xes

( W

m-2

)

Hours

Rn

LE

H

G

Fig. 10. Seasonal variation of energy fluxes. A. May. B. June. C. July. D. August.

Energy balance closure for each month is shown in Fig. 11. The slope of the linear regression is

particularly influenced by the canopy growth. When the field is completely covered by the

vegetation and it can be considered as an homogenous surface, energy balance closure decreases

up to 0.77 with an intercept value of about -1.4 W m-2

. This is probably due to the effect of

canopy and photosynthetic storage terms which become important when the vegetation is tall and

the surface is homogenously covered by the plants. Analyzing each flux of the energy balance

over the whole experimental period (Fig. 10) it is possible to realize that over a field covered by

dense vegetation, latent heat is the main dominant component of the energy budget (respect to

sensible heat and soil heat ground) and a lack of the energy balance closure corresponds to an

underestimation of the canopy evapotranspiration fluxes. In water management practices this

problem assumes a dominant role in irrigation procedure given that a correct estimation of the

evapotranspiration fluxes corresponds to an efficacious and sustainable management of the water

resource.

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59

-1.5

-1

-0.5

0

0.5

1

0.4

0.6

0.8

1

1.2

May June July August

Inte

rcep

t (W

m-2

)

Slo

pe

an

d R

2(-

)

Slope

R2

Intercept

Fig. 11. Energy balance closure evaluated for each month.

Random error

Reliability of turbulent fluxes can be obtained only if theoretical assumption of the eddy

covariance technique, described in Moncrieff et al. (1996), are followed. Non steady-state

conditions, random noise of the signal, inadequate length of sampling interval, size variation of

flux footprint and surface heterogeneity, single point measurement of turbulence and inadequate

sensor response could cause random uncertainty in fluxes measurements. Random errors have

been mainly studied by Hollinger and Richardson (2005) comparing flux measurements obtained

by two identical micrometeorological stations located in the same place with the same flux

footprint, or by Richardson et al. (2006) comparing pair of measurements made on two

successive days from the same tower under equivalent environmental conditions. Using

Lenschow et al. (1994) method to detect random uncertainty in sensible and latent heat fluxes, it

is possible to realize that errors in estimated means, variances and co-variances diminish

increasing the size of data set (as long as the data set is not enlarged that, for example, seasonal

trends become important) and the random uncertainty magnitude proportionally increases with

the growth of sensible and latent heat flux intensities (Fig. 12).

A B

0

10

20

30

40

50

-200 -100 0 100 200 300

Ra

nd

om

un

cert

ain

ity

(W

m-2

)

Sensible heat ( W m-2)

0

20

40

60

80

100

-100 0 100 200 300 400 500

Ra

nd

om

un

cert

ain

ity

(W

m-2

)

Latent heat ( W m-2)

Fig. 12. Random uncertainty in function of sensible (A) and latent (B) heat flux magnitudes.

Some authors as Bernardes and Dias (2010) include error bars when reporting measured values

of turbulent fluxes. It is not a common micrometeorological practice but to realize how random

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60

errors affects latent and sensible heat fluxes, in Fig. 13 the mean daily turbulent flux intensities

jointed with their range of confidence, are shown. The maximum uncertainty is associated with

daytime when maximum latent and sensible heat magnitudes are shown. During daytime, the

maximum range of confidence is about 40 W m-2

for sensible heat and 80 W m-2

for latent heat,

while during the nighttime it tends to zero.

A B

-20

10

40

70

100

130

0 3 6 9 12 15 18 21 24

Sen

sib

le h

eat

(W m

-2)

Hours

H

Random uncertainity

-20

60

140

220

300

380

0 3 6 9 12 15 18 21 24L

ate

nt

hea

t (W

m-2

)

Hours

LERandom uncertainity

Fig. 13. Range of confidence obtained from random error estimation for sensible (A) and latent

(B) heat fluxes.

Generally, some random error sources could be solved trying to apply rigorously practical rules

described in many literature works which have been written starting from the birth of the eddy

covariance technique (Foken, 2008a; Schmid, 1997). However, the energy balance closure is

affected by these errors which can not be completely eliminated. Filtering methods based on a

spatially decomposition of turbulent fluxes (Salesky et al., 2012) tries to quantify rigorously the

random errors with the objective, in the common practice for the authors, to include an estimate

of random errors magnitude when micrometeorological measurements are shown.

Conclusion

Livraga 2012 measurements have been an excellent data set for evaluating the surface energy

balance problems. All findings about the flux error sources cannot completely explain the

problem of the unclosed surface energy balance. It is founded that crucial attention to calibration,

maintenance and software correction of data is essential to obtain half-hourly reliable fluxes.

Despite this effort, data set contains an unbalance of about 25% which has been studied taking

into account different turbulent flux problems.

Storage terms play a fundamental role to improve the energy balance closure and they are about

10% of the daily available radiation energy. Photosynthesis and canopy storage terms are

prevalent in the field when the vegetation covers the soil surface and the canopy is fully

developed. Ground heat storage is greater than the other storage terms and it can reach up to 50%

of the soil heat flux. Canopy growth and seasonality effects are strongly connected with storage

terms. When the vegetation is lowed the energy balance closure is almost equal to 1 because only

ground heat storage term exists with a percentage weight of about 30%. From class C1 to class

C5 the energy balance closure decreases if the vegetation storage terms (canopy and

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61

photosynthesis terms) are not considered. Similarly, energy balance closure decreases from May

to August in accordance with the increasing of the vegetation storage terms. Energy balance flux

partitioning highline how the available energy (net radiation) is subdivided in latent, sensible and

soil heat fluxes, detecting the flux which could mainly contribute to the unbalance problem.

During experimental campaign the results show that latent heat is the main component of the

energy budget, and, in some months, it is grater then 40% of the available energy.

Atmospheric turbulence characteristics play a fundamental role in flux reliable estimations. In

some cases, half-hourly averaged time is not sufficiently longed to take into account the long-

wave terms of the turbulent flux measurements. Studying the ogive functions, the results show

that about 20% of data are partially corrected because their aggregation time covers only a

portion of turbulent eddies which stay in the surface layer (Garrat, 1993). Some authors

(Lenschow et al., 1994) suggests to change the averaged aggregation time of the eddy covariance

flux measurements in function of the atmospheric turbulence characteristics, but increasing

drastically the complexity of the common practice measurements. State of turbulent mixing is an

important aspect against to the advection phenomenon. One of the theoretical assumption of the

eddy covariance technique is that advection terms can be neglected. Friction velocity is used to

give a threshold which discerns the existing probability of the advection transport. Energy

balance closure in developed turbulent mixing conditions is greater than the cases with low

turbulence, and the closure is about 0.8 if friction velocity is confined between 0.24 and 0.83 m

s-1

.

In the past the researches on the energy balance closure problems was mainly directed on

measuring errors, and only a few results underline the scale hypothesis. The results shown in this

work underline the complexity of the source area footprint definition for each flux of the energy

budget. Atmospheric stability conditions, measurement height, surface roughness and wind

velocity are some common parameters which govern the footprint models. In Po Valley, the

weak wind velocities and strong convective forces during summer months provoke the

movement of footprint peak in direction of the tower, so that the major representativeness of

source area is certainly confined inside the field. Site specific new experiments should be made

to understand how the representative source area for eddy covariance measurements change in

function of atmospheric, physical and geometrical characteristics of the field. It should be a

subject of further researches to recalculate eddy covariance experimental results again using a

new experimental plan and a specialized measuring setup calibrated for the scale problem. LES

modeling studies could be used to support these researches.

Despite this overview cannot be a final work, this paper shows important results about the

energy balance closure problem. Moreover, this work is one of the few researches on maize field

in Po Valley which are presented in literature, increasing the knowledge on the energy balance

problems at international scale.

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Wilson, K., Goldstein, A., Falge, E., Aubinet, M., Baldocchi, D., Berbigier, P., et al. (2002). Energy balance closure

at FLUXNET sites. Agricultural and Forest Meteorology , 113: 223-243.

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(Chapter 3) – Experimental data about the spatial variability of scalar fluxes across maize field in Po Valley and

comparison with theoretical footprint model predictions

Abstract

Representative source area for turbulent flux measurements by eddy covariance stations is an

important issue which has not yet been fully investigated. In particular way, the validation of the

analytical footprint models is generally based on the comparison with Lagrangian model

predictions, while experimental results are not largely diffused in literature. In this work, latent,

sensible heat and carbon dioxide flux measurements across two experimental fields in Po Valley

are shown, and two totally different scenarios at bare and vegetated soils are analyzed.

Experiments are performed using two eddy covariance systems: one fixed station which is

located about in the middle of the field and a mobile station which is placed at various distances

from the field edge to investigate the horizontal variation of the vertical scalar fluxes. The

measured fluxes of latent, sensible heat and carbon dioxide are compared with the predictions of

two analytical footprint models. There is a good agreement between measurements and one of

the two analyzed model predictions. The results have also shown that the spatial distribution of

turbulent fluxes is strongly influenced by the presence of vegetation in the field. Moreover, each

turbulent flux is characterized by its own representative source area which could be extremely

different from the others increasing the complexity of the footprint problem determinations for

eddy covariance measurements.

Introduction

Eddy covariance measurements are widely applied to continuously monitor turbulent exchange

of mass and energy at the vegetation-atmosphere interface (Aubinet et al., 2000). Moreover, the

eddy covariance method is one of the most accurate and direct approaches available in literature

to measure turbulent exchanges over field areas with different sizes (Baldocchi et al., 2001). The

eddy covariance method is a statistical tool which, stating from high-frequency data of wind

components and scalar densities, provides to assess latent, sensible heat and carbon dioxide

turbulent fluxes (Baldocchi, 2003). The fluxes are calculated as a covariance among turbulent

components of vertical wind velocity and scalar concentration (vapor, air temperature or carbon

dioxide). The main micrometeorological instruments which give the name to the eddy covariance

technique are the tridimensional sonic anemometer and gas analyzer respectively. The reliability

of flux measurements depend on certain theoretical assumptions of the eddy covariance

technique (Kaimal and Finnigan, 1994; Foken and Wichura, 1996), the most important of which

are horizontal homogeneity, stationarity and mean vertical wind speed equal to zero during the

averaging period. Eddy covariance method was used in micrometeorology for over 30 years, and

now, modern instruments and software make this method easily available and widely used in

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different research fields, such as in ecology, hydrology, environmental and industrial monitoring

(Baldocchi et al., 1988; Papale et al., 2006).

In the past years a global network of micrometeorological tower sites which use eddy covariance

methods to measure carbon dioxide, water vapor and energy exchanges between soil-vegetation

and atmosphere systems was constituted. Its name is Fluxnet and as of January 2009, there are

over 500 tower sites in continuous long-term operation

(http://www.fluxnet.ornl.gov/fluxnet/overview.cfm, Wilson et. al., 2002; Sanchez et. al., 2010).

The proliferation of eddy covariance flux systems in a variety of conditions and ecosystems,

often violating some the theoretical requirements of the methodology, has created an increasing

interest in footprint analysis (Schmid, 1997; Rannik et al., 2000). Schuepp et al. (1990) specify

the term ‘footprint’ as the relative contribution from each element of the upwind source area to

the measured concentration or vertical flux. It can be interpreted as the probability that a trace

gas, emitted from a given elemental source, reaches the measurement point. Mathematically, flux

and footprint are related by Eq. 1 as explained in Hsieh et al. (2000).

x

mm dxzxfxSzxF ),()(),( (1)

Where F is the scalar flux, f is the footprint function, S is the source strength, zm is the

measurement height and x represents the horizontal coordinate along wind direction.

As described in Vesala et al. (2008), the determination of the footprint function is not a

straightforward task and several theoretical approaches have been derived over the previous

decades. They can be classified into four categories: (i) analytical models, (ii) Lagrangian

stochastic particle dispersion models, (iii) large eddy simulations, and (iv) ensemble-averaged

closure models. Additionally, parameterizations of some of these approaches have been

developed, simplifying the original algorithms for use in practical applications (e.g., Horst and

Weil, 1992; Schmid, 1994). The criterion of a 100:1 fetch to measurement height ratio was long

held as the golden rule guiding internal boundary layer (IBL) estimation and nowadays is still

used as a rule-of- thumb to crudely approximate the source area of flux measurements over short

canopies in daytime conditions. However, the unsatisfactory nature of the 100:1 ratio and the

related footprint predictions were explicitly discussed by Leclerc and Thurtell (1990).

The dramatic increase of publications that address footprint modeling, applications or related

issues of fetch and spatial representativeness for flux measurements in recent years, demonstrates

the growing need for practical footprint models. The development of a growing number of long-

term trace gas exchange studies over complex forest canopies and in often topographically

challenged terrain, underlines the fact that the requirements for future footprint models are

divergent: on the one hand, practical footprint models must be easy to use, if ever possible in the

field, where the availability of computer resources (and time) is limited. The recent

developments in analytical footprint models satisfy this need, but these models are limited to

homogeneous surface layer similarity conditions (Horst and Weil, 1992; Schuepp et al., 1990;

Hsieh et al. 2000; Kormann and Meixner, 2001). On the other hand, footprint models should

produce realistic results in real-world situations for measurements over (or below) tall canopies,

spatially heterogeneous turbulence, stability conditions from extremely stable to free-convective,

and instationarity. Backward Lagrangian models and the large eddy simulation-based footprint

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68

studies provide for the analysis of the representativeness source area in real-world situations but

also if they are considered promising, computational time and extreme complexity restrict their

application field (Kljun et al., 2002; Rodean, 1996; Wilson and Sawford, 1996; Thomson, 1987).

There is a general need for footprint model validations. According to Foken and Leclerc (2004)

only a few experimental data set are available for validation proposes. Lagrangian dispersion

models are tested against dispersion experiments of artificial traces for different turbulence

regimes (Thomson, 1987; Kurbanmuradov and Sabelfeld, 2000; Kljun et al., 2002; Leclerc et al.,

2003). Measurements in complex flow fields, as dispersion inside and above high vegetation

canopy, may not be ideal for evaluation and validation of footprint models. Kljun et al. (2004)

suggest the validation under ideally controlled conditions that can be reproduced in wind tunnels.

Generally, analytical footprint predictions are often evaluated using results of Lagrangian

footprint models. Nowadays, only sites with short vegetation and an accurate selection of

measured data, according to the quality check criteria by Foken and Wichura (1996), allow the in

situ validation of analytical footprint models in “nearly ideal” conditions. In Marcolla and

Cescatti (2005) a new approach for the determination of the relative contribution of a source area

to the measured turbulent flux is shown. In their study areas at different distances from the

measuring point are cut at different times, thus generating spatial and temporal variability in the

sink strength. Light response curves at three different time periods, characterized by

homogenous or heterogeneous surface coverage, are used to quantify the contribution of the area

within a certain distance from the measuring system to the total flux. Gockede et al. (2005)

approach is constituted by two flux stations over bare soil and a meadow. A third station, with a

footprint area covering both surfaces, is used to validate the footprint model, because the

contributions of both surfaces changed with the stability and wind velocity. Earlier investigations

used a similar approach: Soegaard et al. (2003) operated five ground-level eddy covariance

systems over five different crop fields together with a sixth set-up on top of a higher mast to

enable landscape-wide flux measurements. The agreement between high-level values and those

integrated from ground-level using a re-formulated version of the models of Gash (1986) and

Schuepp et al. (1990) is good. Van de Boen et al. (2013) use a data set obtained by three eddy

covariance stations located in landscape with different land use typologies, to test the

performance of the Hsieh et al. (2000) and Kormann and Meixner (2001) footprint models using

an experimental methodology widely described in Neftel et al. (2008). In literature, only one

experiment which investigates the horizontal variation of the vertical turbulent fluxes over a

potato field is shown (Baldocchi and Rao, 1995). The experiment is performed by placing a

mobile eddy covariance station at various distances from the upwind field edge versus a fixed

eddy covariance station located in the middle of the field. The results are used by Hsieh et al.

(2000) to validate their footprint model starting from natural traces.

In this paper Baldocchi and Rao (1995) methodology to validate Hsieh et al. (2000) and

Kormann and Meixner (2001) footprint models has been proposed again but, for the first time, it

is applied over two experimental fields located in Po Valley: one characterized by bare soil and

another one covered by maize plants. Particular wind condition regimes, atmospheric turbulence

characteristics and field geometrical shapes, which occur in Po Valley, make of this experiment

an interesting footprint model validation proof. This paper describes experimental set up and its

execution, furthermore, the results about intra-field spatial variability of latent, sensible and

carbon dioxide fluxes are compared with Hsieh et al. (2000) and Kormann and Meixner (2001)

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69

footprint models to verify their reliability also for eddy covariance station placed over Padana

region cultivations.

What is the importance of this experiment?

In this paragraph many different improvement connected with a correct definition of the

representative source area for turbulent flux measurements are briefly summarized.

1) Representative source area for turbulent fluxes has to be confined inside the field if the

eddy covariance flux measurements are used to characterize water management practices

or canopy phenological growth. In Po Valley, where the field shapes are quite small (in

the order of ten hectares), rigorous footprint modeling predictions are necessary to reduce

uncertainty over the evapotranspiration flux representative source areas. Footprint model

validations could also contribute to improve the reliability of turbulent flux

measurements by eddy covariance stations decreasing the uncertainty about

evapotranspiration annual budget over cultivated fields.

2) This experiment actively contributes to improve literature results about footprint model

validation experiments with a scenario totally different by the other presented nowadays

in literature. Moreover, as highlighted by Foken and Leclerc (2004), many experimental

campaigns to validate footprint models are expensive, and hence prohibitive for the vast

majority of university researches. Increasing literature experimental results, which try to

resolve this problem, a common database could be developed so that it can be consulted

by the researcher for their experiments.

3) Flux spatial distribution results above the canopy or on bare soil can be used in some

mathematical models, from Lagrangian stochastic dispersion to large eddy simulation, to

describe in an accurate way the field-domain turbulent real conditions, comparing output

model results with the experimental measurements.

4) The knowledge about representative source areas for latent and sensible heat fluxes could

contribute to resolve the energy unbalance problem which can be seen as a scale problem

about sensor measurements as widely discussed in Foken (2008).

5) Another practical implication about footprint model validations is connected with the

correct definition of the eddy covariance tower position in the field. In fact, it has to be

located sufficiently far from the field edge to avoid the influence of the neighbor fields.

However, eddy covariance measurements which are performed in fields where the

heterogeneity is particularly accentuated, need to known the footprint shape and its size

to understand the weight of fluxes which come from the neighbor fields.

These points explain five macro-areas which could be affected by the results of this experiment,

making a list about the problems which many scientists met in their researches.

Theoretical background

Estimation of flux footprint from experimental data is compared with predictions of two

analytical footprint models proposed by Hsieh et al. (2000) (called Hsieh model) and Kormann

and Meixner (2001) (called Kormann Model). The choice of these footprint models is a

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70

compromise between reliability and simplicity, following the suggestion by Foken and Leclerc

(2004) on the necessity of easy-to-use footprint models.

Hsieh et al. (2000) model is constituted by a combination of Lagrangian stochastic model results

and dimensional analysis. It analytically relates atmospheric stability, measurement height and

surface roughness length to obtain an approximated analytical expression which accurately

describes the footprint function. The results are organized in non-dimensional groups and related

to the input variables by regression analysis. The advantages of this model are evident: the

hybrid model can be expressed by a set of explicit algebraic equations, while some of the

complexity and skill of the full model is retained through the regression. However, the pitfall of

any approximation or parameterization is that its validity is strictly limited to the range of

conditions over which it is developed.

Kormann and Meixner (2001) model belongs to the class of the Eulerian analytic flux footprint

models which explore several approaches to approximately resolve the advection-diffusion

equation. Schuepp et al. (1990) are the first scientists that have taken a purely analytical

approach, based on an approximate solution of the diffusion equation given by Calder (1952) for

thermally neutral stratification and a constant wind velocity profile. As stated by the authors, it

suffers from the restriction to neutral stratification. Their suggestion, to correct the wind velocity

in the footprint calculation based on thermal stability, has no mathematical basis. Instead,

Kormann and Meixner (2001) model includes parameterizations of power law for wind velocity

and eddy diffusivity extending the applicability of their footprint model to the whole atmospheric

stability range. However, some model limitations are present, such as its usage in areas where

wind velocity and eddy diffusivity profiles are horizontally homogeneous, and at heights where

the effects of a finite mixing depth are negligible. In addition, this model assumes that turbulent

diffusion in streamwise direction is small compared to advection, a form of Taylor’s hypothesis,

and are thus confined to flow situations with relatively small turbulence intensities.

Hsieh Model

Hsieh et al. (2000) develops an approximate analytical model to estimate the flux footprint in

thermally stratified flows. This is a hybrid approach combining elements from Calder’s

analytical solution (1952) with the results of Thompson’s Lagrangian model (1987). In the

analysis of their results, they scaled Gash (1986) effective fetch with the Obukhov length and

accounted for the effect of stability introducing two similarity parameters D and P, obtaining the

Eq. 2.

P

u

L

zD

SFkL

x

||)/ln(

1

|| 0

2 (2)

Where zu is a length scale, function of measurement height and surface roughness. k is the Von

Karman constant , L the Obukhov length and D and P depends on stability conditions of the

atmosphere . F/S0 is the ratio between scalar flux and source strength always confined between 0

and 1 (Hsieh et al., 2000).

The footprint function is expressed by Eq. 3.

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71

PPu LDz

xkPP

um eLDzxk

zxf

1

2||

1

1

22||

1),( (3)

Kormann Model

The Kormann Model is based on a modification of the analytical solution of the advection-

diffusion equation of Van Ulden (1978) and Horst and Weil (1992) for power low profiles of the

mean wind velocity and the eddy diffusivity. To allow for the analytical treatment, the model

assumes homogenous and stationary flow conditions over homogeneous terrain, it represents the

vertical turbulent transport as a gradient diffusion process and it considers only advection in

along wind direction. Assuming that vertical and crosswind dispersion are independent, the

continuity equation reduces to a two-dimensional advection-diffusion equation.

In the Kormann Model the footprint function is expressed by Eq. 4.

xr

z

xr

z

r

mx

zxfK

r

mur

m

K

r

mum 2

1

2exp

1

1),( (4)

Where is the gamma function, r the shape parameter related to the exponents of the power

laws as r=2+m-n (Van Ulden, 1978) and Ku , are proportionally constants determined by

fitting the power laws for u ( m

u zu ) and K ( n

K zK ) to Monin-Obukhov similarity theory

(Garrat, 1993).

Study site, instruments and data

In this paragraph, filed characteristics, instruments necessary to perform the experiments and

data corrections are briefly shown.

Site characteristics

The experiments are carried out in two fields destined for maize cultivations at Landriano (Pavia,

Italy) and Livraga (Lodi, Italy) respectively. Fields geographic coordinates are (45.19 N, 9.16 E,

87 m a.s.l.) and (45.11 N, 9.34 E, 61 m a.s.l.) for Landriano (Field 1) and Livraga (Field 2)

respectively. The experiments are performed in two different situations: after reaping time (Field

1) and during maximum phenological development of the homogenous maize canopy (Field 2).

Both fields have a polygonal shape with a flat area of about ten hectares large. Field 1 is

completely surrounded by tall row plants which generate a strong discontinuity with the

neighbouring fields, while Field 2 is surrounded on three sites by other maize fields and in

South-West direction it forms a border with an uncultivated zone.

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Instruments

With objective to investigate evapotranspiration and carbon dioxide fluxes over maize

cultivation in Po Valley, in the middle of Field 1 and 2, fixed eddy covariance towers A1 (for the

Field 1) and A2 (for the Field 2) are installed, and here, instruments are briefly summarised.

The stations are equipped with the following sensors: one three-dimensional sonic anemometer

(Young 81000), which measures sonic temperature and three components of wind speed at the

height of 5 m; one open-path gas analyzer (LICOR 7500) which measures water vapour and

carbon dioxide concentrations at the height of 5 m too. Both these instruments have been set with

an acquisition frequency of 10 Hz, so that the data can be used to calculate latent, sensible heat

and carbon dioxide fluxes trough eddy covariance method. One net radiometer (CNR1 by Kipp

& Zonen) is located on an arm (2.5 m long) attached on the tower at the height of 4 m. One

thermo-hygrometer (HMP45C Campbell Scientific) is located at the height of 3.5 m to measure

air humidity and temperature. In the soil, two thermocouples (by ELSI) and a heat flux plate

(HFP01 by Hukseflux) are placed at a depth of about 10 cm. Contemporaneously, soil moisture

is detected by three humidity probes (CS616 by Campbell Scientific) at different depths. Finally,

one rain gauge (AGR100 by Campbell Scientific) is separately located by the tower and, at the

height of about 1.5 m, it measures the precipitation intensity.

Data logger CR5000 (Cambpell Scientific) is used to store all data with an averaged time step of

5 minutes. This averaged time is designed to ensure that the eddy flux measurement system

captures most of the flux-containing eddies. This goal was accomplished by sampling

anemometer and gas analyzer sensors rapidly and averaging data over a time step of 5 minutes.

This averaged time is also justified by the results obtained by Masseroni et al. (2012) which,

studying surface layer turbulent characteristics over the Field 1, show that eddy integral lengths

in convective situations tends to be stationary for a time major of 300 s (about 5 minutes).

Data corrections

Energy fluxes have been corrected applying the whole range of correction procedures described

in many different literature works (Aubinet et al., 2000; Foken et al., 2004; Mauder and Foken,

2004). Before calculating fluxes, two groups of correction have been applied: “instrumental” and

“physical” corrections. Axis rotation for tilt corrections, spike removal, time lag compensation

and detrending represent preliminary processes which have to be directly applied on high

frequency measurements to prepare the data set for fluxes calculation. Spectral information

losses as a consequence of measurement system typologies trough transfer function

characteristics and sampling errors, have to be opportunely corrected to compensate the

underestimation of the turbulent fluxes (Moncrieff et al., 1997). Moreover, air density

fluctuations and air humidity effects on sonic temperature have to be necessarily corrected

trough Webb et al. (1980) and Van Dijk et al. (2004) procedures respectively.

These instrumental and physical corrections are automatically implemented in a PEC (Polimi

Eddy Covariance) software which has been opportunely developed for this experiment by

Corbari et al. (2012). The core of software is based on four substantial points:

a) Data stored into the data logger are sent on specific computer at the Politecnico of Milan

using a GSM modem;

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b) Automatically, correction algorithms are activated and turbulent fluxes are calculated;

c) Some statistic indexes are generated to control the micrometeorological variables;

d) Turbulent flux and micrometeorological variable graphics are plotted at the web page

http://geoserver.iar.polimi.it.

Fixed eddy covariance stations (A1 and A2)

Energy flux measurements are proper to the cultivation if eddy covariance station is correctly

positioned inside the field. It has to be opportunely located far from the field edges, so that flux

measurements do not belong to the neighboring fields. Moreover, anemometer and gas analyzer

have to be compatible with the constant flux layer (Savelyev and Taylor, 2005). The constant

flux layer represents a space area where eddy covariance station measurements are constant, and

it is defined as 10-15% of internal boundary layer (Baldocchi and Rao, 1995). Considering the

whole wind direction ranges and analyzing the bare soil unfavourable conditions where

aerodynamic roughness for both fields is about 0.041 m, the constant flux layer depth at the

towers A1 and A2, calculated trough Elliot (1958)’s formula, is about 6 m ensuring that

anemometer and gas analyser are included into the constant flux layer. Moreover, several

conditions should be met before eddy correlation method can be applied to measure the fluxes of

mass and over an experimental field. First, the site should be flat. Second, vertical velocity

should be measured normal to the surface streamlines. Third, the crop should be homogeneous

and sufficiently extensive. Finally, no intermediate or advective sources or sinks should be exist

for the scalar under inverstigation (Baldocchi et al., 1988).

A method which is generally used to confirm the reliability of turbulent flux measurements of an

eddy covariance station is the energy balance closure (Foken et al., 2006). However, energy

balance issue is still unresolved problem and the closures which are present in literature

generally vary from 0.5 to 0.98 (Foken, 2008). The slope of the regression line between latent

and sensible heat turbulent fluxes and ground heat flux against available energy (net radiation) is

performed over Field 1 and 2 and the results are shown in Fig. 1.

0.84

0.91

0.98

1.05

1.12

1.19

0.72

0.76

0.80

0.84

0.88

A1 A2

Inte

rcep

t (W

m-2

)

Slo

pe

an

d R

2(-

)

Slope

R2

Intercept

Fig. 1 Energy balance closure for fixed eddy covariance stations A1 and A2.

Intercept and correlation coefficient (R2) are also included in Fig. 1, to highlight the presence of

systematic or random errors. The energy balance closure for A1 and A2 stations is about equal to

0.8 with a low dots dispersion around the regression line and a negligible systematic error of

about 1 W m-2

.

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Experimental execution

Experimental campaigns were carried out in two consecutive years: 2011 and 2012 respectively.

For the Field 1 the experiment was performed over a range of nine days, from 15 September to

23 September in the year 2011, while for the Field 2 the experiment was performed over a range

of six days, from 2 August to 8 August in the year 2012.

In Tab.1 and 2 four daily averaged atmospheric parameters measured by the eddy covariance

stations over the experimental periods, are shown. The fields, which are at a distance of about 50

Km, are characterized by similar atmospheric turbulent conditions. Weak wind velocities, which

are typical in Po Valley, have a range which vary between 0.7 and 3 m s-1

. Friction velocities are

quite constant at a value of about 0.1 m s-1

. Air temperatures are greater than 20 °C in

accordance with the seasonal mean temperatures. Net radiations are grater then 200 W m-2

except for 261 and 262 Julian days of the year 2011 where the sky were particularly covered by

clouds.

Tab. 1. Meteorological conditions measured by A1 eddy covariance station in the year 2011.

Julian

day

Mean

velocity

(m s-1

)

Friction

velocity

(m s-1

)

Air

Temperature

(°C)

Wind

direction

(°)

Net

radiation

(W m-2

)

258 0.71 0.085 22.15 212 269

259 0.79 0.090 22.45 239 236

260 1.40 0.16 21.34 251 298

261 1.59 0.15 19.14 197 93

262 2.84 0.26 15.04 250 186

263 1.13 0.12 15.33 202 291

264 1.02 0.11 16.86 225 284

265 0.79 0.10 18.43 206 292

266 1.65 0.23 21.91 122 243

Tab. 2. Meteorological conditions measured by A2 eddy covariance station in the year 2012.

Julian

day

Mean

velocity

(m s-1

)

Friction

velocity

(m s-1

)

Air

Temperature

(°C)

Wind

direction

(°)

Net

radiation

(W m-2

)

215 1.01 0.12 25.69 230 310

216 0.93 0.10 25.42 210 301

217 1.09 0.15 24.73 250 297

218 1.11 0.13 24.98 239 285

219 1.81 0.17 25.97 247 307

220 1.16 0.16 25.01 290 304

To investigate the horizontal variation of turbulent fluxes across the fields, the experiments are

performed by placing a mobile eddy covariance station (B1 for the Field 1 and B2 for the Field

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2) at various distances from the field edge, moving it versus the fixed stations (A1 or A2) placed

about in the middle of the fields. The mobile stations (Fig. 2A and B) are equipped by a sonic

anemometer (Young 81000) as well as the open-path gas analyzer (LICOR 7500) which are

attached at the top of an extensible tripod. To verify if mobile station measurements are equal to

those obtained by fixed stations, both stations have been placed close together for some days

before the experiments. Moreover, the clock among two data loggers (CR5000 for B1 and

CR23X for B2) has been set to obtain measurements at the same time.

A B

Fig. 2. Mobile stations in the Field 1 (A) and in Field 2 (B). In (A) fixed tower A1 is also shown.

In the Field 1, the mobile system (B1) is placed at nominal distances of 0 (P1_1), 15 (P2_1) and

65 (P3_1) meters from the field edge along a reference line inclined of about 191° in respect to

North. In the Field 2, the mobile system (B2) is placed at nominal distances of 0 (P1_2), 14

(P2_2) and 50 (P3_2) meters from the field edge along a reference line inclined of about 236° in

respect to North. The fixed towers (A1 and A2) are placed at a distance of the field edge of about

184 and 188 meters respectively (Fig. 3).

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A B

North

South

East West (A1)

(B1)

191

40

North

East West

South

(A2) 236

(B2)

40

Fig. 3. Maps of the experimental sites. (A) Field 1 and (B) Field 2. The circle indicates the fixed

stations (A1 or A2) while the triangles the mobile station positions. The dotted line indicates the

reference line.

Latent, sensible heat and carbon dioxide flux measurements performed by mobile stations are

compared with those which are contemporaneously obtained by the fixed stations, but only a

range of data is taken into account for the analysis. Data are selected only when wind directions

are included in a range of 40° in respect to the reference line (Fig. 3) and net radiation is greater

than 0 W m-2

(Baldocchi and Rao, 1995). For this reasons, the experimental period cover several

days because mobile towers can not be moved as long as a sufficient number of data have been

stored.

The experiment success is guarantee if the field has at least one border site with a strong

discontinuity in respect to the examined field typology, and the reference line has to be

orientated in respect to this discontinuity zone (Fig. 3). Moreover, the fluxes which come from

the upwind zones in respect the discontinuity border should be quite constant during the whole

experimental period. To verify this condition, mobile station has been stayed on field border for

some days before the experimental campaign and the results have shown that daily averaged

fluxes does not drastically change from day to day.

Results

In this paragraph experimental measurements are compared with theoretical footprint models,

and some considerations about footprint model reliabilities have been discussed.

Flux measurements across the fields

To investigate latent, sensible heat and carbon dioxide spatial distribution across the Filed 1 and

2, eddy covariance measurements performed by B1 and B2 mobile stations have been compared

with those obtained by A1 and A2 fixed stations. In practice, mobile station measurements have

been normalized with fixed station measurements for each steady point of the experimental

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design. Moreover, experimental data have to be rigorously processed with the goal to compare

experimental measurements with theoretical footprint model results.

The starting point for experimental data processing is dictated by the slope determination of the

regression line for the ratios between mobile and fixed station measurements for each

measurement point. For example, when the mobile station B1 stays at P1_1 point, on a Cartesian

plane B1 and A1 station measurements are plotted together in order to calculate the regression

line between mobile and fixed measurements. The slope of the regression line which has been

determined trough this method, represents the first point in the Fig. 4A and B. F can be

considered as a mean latent heat (Fig. 4A) or carbon dioxide (Fig. 4B) flux measurement

performed by the mobile system for the whole period where the station stays in a specific point,

while SA is that performed by the fixed station for the same period. F/SA ratio is a variable which

theoretically varies from zero to one. However, at P1 points (both in the Field 1 and 2), the

upwind fluxes are not zero and the F/SA ratio always starts with a value which is about 0.4 for

latent heat and carbon dioxide concentrations. Only in one case (Field 1) carbon dioxide

experimental measurements lead to having regression line with a slope near to zero. The last

point in Fig. 4A and B, which corresponds at P3_1 or P3_2 position, is equal to one because

mobile and fixed station are in the same position and the flux measurements are equivalent.

A B

0.0

0.4

0.8

1.2

0 50 100 150 200

F/S

A(-

)

Distance from the field edge (m)

LE_Field 1

LE_Field 2

0.0

0.4

0.8

1.2

0 50 100 150 200

F/S

A(-

)

Distance from the field edge (m)

f_CO2_Field 1

f_CO2_Field 2

Fig. 4. Turbulent flux measurements across the fields. (A) latent heat (LE), (B) carbon dioxide

flux (f_CO2). F/SA represents the ratio between mobile and fixed station flux measurements.

In the Field 1 and 2 the upwind zones have a sensible heat major then experimental fields, so that

the slope of the regression line is certainly greater than one. Therefore, to obtain the F/SA ratio

point distributions as shown in Fig. 5, the ideal case where mobile and fixed measurements are

equivalent with a slope of the regression line equal to 1, has been subtracted from the real value

of the slope (major then 1) and successively this result is again subtracted to 1. As shown in Fig.

5, sensible heat at the field border is quite different from Field 1 to 2. In bare soil F/SA ratio is

near to 0.4 as similarly shown for latent and carbon dioxide fluxes in Fig. 4A and B respectively,

while when high vegetation is opposed with an uncultivated zone, at the transition point (P1_2),

mobile and fixed station measurements are totally different and the F/SA ratio is about equal to

zero.

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78

0.0

0.4

0.8

1.2

0 50 100 150 200F

/SA

(-)

Distance from the field edge (m)

H_Field 1

H_Field 2

Fig. 5. Sensible heat flux measurement across the fields. F/SA represents the ratio between

mobile and fixed station flux measurements.

The results obtained in these experimental campaigns and globally summarized in Fig. 4 and 5,

have shown that flux distributions across the fields are in accordance with the prediction

described in Baldocchi and Rao (1995)’s work. In the Field 2 latent, sensible heat and carbon

dioxide fluxes have a quite standard logarithmic behavior, while in the Field 1 this trend is

verified only for the latent heat. In the Field 1, sensible heat is quite influenced by the boundary

conditions, given that F/SA ratio at P2_1 point is very similar to that in P1_1 position, while for

carbon dioxide flux a linear growth trend is shown. When the canopy homogeneously covers the

field, boundary condition effects can be neglected if the mobile station is beyond from the field

edge of about 50 meters where the F/SA ratio values are already constant and near to 1. For latent

and sensible heat fluxes a similar behavior is also verified in bare soil while the carbon dioxide

flux constantly increases across the field.

Experimental results have shown that turbulent flux magnitudes rapidly increase in a transition

region which is about 50 meters large and then the F/SA ratios can be considered constant to 1 up

to the position of the fixed towers. However, the flux spatial distribution across the field is quite

different for latent, sensible and carbon dioxide fluxes, and it is strongly influenced by the

presence of the canopy on the soil.

Experimental data compared with footprint model predictions

In this subparagraph footprint model predictions are matched with latent, sensible heat and

carbon dioxide flux measurements across the experimental fields. In both sites the upwind fluxes

outside the fields are not zero and the source strength shown in Eq. 1 is simply approximated by

the Eq. 5.

0

0)(

1

xforS

xforSxS

A

(5)

Where S1 and SA are the fluxes measured by eddy stations at zero meters and at the position of

the fixed towers respectively. By superposition, it is possible to calculate the flux ratio using the

methodology widely described in Hsieh et al. (2000) and synthetically explained by Eq. 6.

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x

m

x

m

AA

m dxzxfdxzxfS

S

S

zxF

0

1 ),(),(),(

(6)

In this way, theoretical footprint models can be compared with experimental measurements, and

the results are globally shown in Fig. 6 and 7. Each averaged data of flux is characterized by its

own representative source area which is defined by the F/SA ratio which is calculated trough Eq.

6. The data which are used into Eq. 6 have been measured by the fixed stations over the whole

period of time of the two experimental campaigns. The range of F/SA values which are obtained

by the fixed station experimental measurements is subdivided in groups each of which covers a

period of time which corresponds to the time period where the mobile station stays at P1, P2 or

P3 positions in the field. Subsequently, the mean of F/SA values for each group has been

calculated, so that F/SA measured and calculated results can be compared.

Fig. 6 and 7 are subdivided in two parts, the first (A, B, C) where the theoretical footprint model

results are matched to the experimental measurements, and the second part (D, E, F) where a

scatter plot defines if the footprint models are in a good agreement with the experimental results.

A B C

0.0

0.4

0.8

1.2

0 50 100 150 200

F/S

A(-

)

Distance from the field edge (m)

Experimental data

Hsieh Model

Kormann Model

0.0

0.4

0.8

1.2

0 50 100 150 200

F/S

A(-

)

Distance from the field edge (m)

Experimental data

Hsieh Model

Kormann Model

0.0

0.4

0.8

1.2

0 50 100 150 200

F/S

A(-

)

Distance from the field edge (m)

Experimental data

Hsieh Model

Kormann Model

D E F

0.0

0.2

0.4

0.6

0.8

1.0

1.2

0.0 0.2 0.4 0.6 0.8 1.0 1.2

F/S

AM

od

eled

(-)

F/SA Measured (-)

Hsieh Model

Kormann Model

0.0

0.2

0.4

0.6

0.8

1.0

1.2

0.0 0.2 0.4 0.6 0.8 1.0 1.2

F/S

AM

od

ele

d (

-)

F/SA Measured (-)

Hsieh Model

Kormann Model

0.0

0.2

0.4

0.6

0.8

1.0

1.2

0.0 0.2 0.4 0.6 0.8 1.0 1.2

F/S

AM

od

eled

(-)

F/SA Measured (-)

Hsieh Model

Kormann Model

Fig. 6. Variation of latent, sensible heat and carbon dioxide fluxes in the Field 1 with the

distance from the field edge, and comparison with theoretical footprint models (A, B, C).

Comparison between measured and modeled model predicted footprint (F/SA). The 1:1 line is

also shown.

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A B C

0.0

0.4

0.8

1.2

0 50 100 150 200

F/S

A(-

)

Distance from the field edge (m)

Experimental data

Hsieh Model

Kormann Model

0.0

0.4

0.8

1.2

0 50 100 150 200

F/S

A(-

)

Distance from the field edge (m)

Experimental data

Hsieh Model

Kormann Model

0.0

0.4

0.8

1.2

0 50 100 150 200

F/S

A(-

)

Distance from the field edge (m)

Experimental data

Hsieh Model

Kormann Model

F E D

0.0

0.2

0.4

0.6

0.8

1.0

1.2

0.0 0.2 0.4 0.6 0.8 1.0 1.2

F/S

AM

od

eled

(-)

F/SA Measured (-)

Hsieh Model

Kormann Model

0.0

0.2

0.4

0.6

0.8

1.0

1.2

0.0 0.2 0.4 0.6 0.8 1.0 1.2

F/S

AM

od

eled

(-)

F/SA Measured (-)

Hsieh Model

Kormann Model

0.0

0.2

0.4

0.6

0.8

1.0

1.2

0.0 0.2 0.4 0.6 0.8 1.0 1.2

F/S

AM

od

eled

(-)

F/SA Measured (-)

Hsieh Model

Kormann Model

Fig. 7. Variation of latent, sensible heat and carbon dioxide fluxes in the Field 2 with the

distance from the field edge, and comparison with theoretical footprint models (A, B, C).

Comparison between measured and modeled model predicted footprint (F/SA). The 1:1 line is

also shown.

In the Field 1, the latent, sensible heat and carbon dioxide variation in spatial distribution, leads

to an unsatisfactory definition of a unique footprint model which can be used to describe the

representative source area for the whole range of turbulent fluxes. In fact, while the agreement

between Kormann model and experimental data of latent heat flux is good, the same could not be

said for sensible heat and carbon dioxide fluxes. Evaluating the errors between model and

experimental results trough the regression line of the dots in the scatter plots, Kormann Model

can be considered the best one for latent heat flux with a slope of the regression line equal to

0.98. However, both models are inadequate to describe footprint shape for sensible heat and

carbon dioxide fluxes with an estimated error of about 10% and 30% respectively.

In the Field 2, latent, sensible heat and carbon dioxide spatial distribution are quite similar. F/SA

ratios have a rapidly increase versus the maximum admissible value of 1 which has been reached

in a transition zone of about 50 meters. Hsieh Model underestimates footprint shape for the

whole range of turbulent fluxes with an error which varies from 5% al 27% for latent and

sensible heat fluxes respectively. Korman Model is in a good agreement with latent heat and

carbon dioxide experimental data with a slight error of about 2%, while for sensible heat Korman

Model underestimates the representative source area with an error of about 20%.

Discussions

Spatial distribution of turbulent fluxes across the field is particularly influenced by the presence

of vegetation which covers the ground surface. In bare soil, boundary condition effects can

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81

remain for several meters away the field edge while, when the vegetation cover the field, the

homogeneity effect of the canopy produces a rapid change in flux distribution leading to 1 the

F/SA ratio at a distance of about 50 meters from the field edge.

The results obtained in Field 1 and 2, have shown that representative source area is not equal for

each flux. Generally, footprint models describe the representative source area for turbulent flux

without specifying if it is latent, sensible heat or carbon dioxide. Experimental results show that,

especially in bare soil, intra-field spatial distribution of turbulent fluxes change from a

logarithmic behavior for latent heat to a linear growth for carbon dioxide. On the other hand, in

Field 2, the F/SA logarithmic growth profile is guaranteed for the whole range of turbulent fluxes,

but the F/SA ratio values are not identical.

Kormann Model could be considered the best one for the whole range of turbulent fluxes,

however also Hsieh Model is in a good agreement with latent heat flux distributions. In the other

cases, Hsieh Model underestimates the footprint area and this is probably due to the simplified

parameterizations which form the model structure. On the other hand, Kormann Model, which

derives from a direct analytical solution of the diffusion equation, approximates footprint area of

the turbulent fluxes in a good way also if, in some cases, it result to be underestimated in respect

to the experimental measurements. The good agreement of the Kormann Model can be due to

atmospheric and turbulent conditions which are typical in Po Valley and which are in accordance

to the limitations and basic hypothesis which govern the theoretical model.

Conclusion

In this work a simple method which is quite different from those recently presented in literature

is used to analyze horizontal variability of vertical scalar fluxes across bare and vegetated soils in

Po Valley. One mobile eddy covariance station is moved from the field edge to the center of the

field where a fixed station is located. Comparing flux measurements obtained by the both

stations, latent, sensible heat and carbon dioxide flux intra-field distributions are investigated and

two footprint model perditions have been compared. A good agreement of the Kormann model is

verified with experimental measurements while Hsieh Model could be used to define footprint

shape only for latent heat flux. Variability of scalar fluxes across the fields is particularly

influenced by the presence of the vegetation and in bare soil turbulent flux spatial distributions

are highly differenced from flux to flux.

These results have contributed to improve the knowledge about the reliability of analytical

footprint model predictions in order to understand the model behaviours over a wide variety of

natural situations where eddy covariance stations could be located. Po valley and its typical

cultivations such as maize or rice are still poorly investigated, but the improvement in eddy

covariance technique, and its applications over a wide range of fields, needs to know more

accurately the representative source areas of the evapotranspiration or carbon dioxide fluxes to

improve management practice in water irrigation or plant care.

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General Conclusion

In this PhD thesis, the complexity of the eddy covariance measurements for turbulent flux

estimations has been investigated with the objective to improve evapotranspiration and carbon

dioxide flux reliabilities. Experimental data corrections, energy balance closure and turbulent

fluxes scales are the main problems which have been widely discussed in literature from the birth

of the eddy covariance technique. Despite the scientific community efforts, some of these

problems have not yet been resolved, and the research in micrometeorological fields should try

to give response on these key points.

The results of this research have shown some important considerations about the possibility to

directly use 30 minutes averaged data to obtain evapotranspiration and carbon dioxide reliable

fluxes. Although the eddy covariance technique requires high frequency data to obtain reliable

covariances and successively turbulent fluxes, PEC software implemented at the Politecnico of

Milan gives the possibility to directly obtain reliable flux estimation starting from the averaged

data in output from data logger. Corrections for air density fluctuations and humidity effects

represent the core of the PEC software and they could be considered the main basis for accurate

flux estimation.

Energy balance closure is generally used to verify the reliability of latent and sensible heat flux

measurements by an eddy covariance station. In an ideal ecosystem, the sum of turbulent fluxes

and ground heat flux should be equal to the available energy (net radiation), but in the real case

the energy balance closure is always lower than one. The results have shown that storage terms

are the main factors which play a substantial role in eddy flux underestimations, and when the

field is homogeneously covered by the canopy, their effect can not be neglected. Ground heat

storage plays a fundamental role in energy balance closure when the field is in bare soil

conditions, while when the vegetation covers the field, photosynthetic and canopy storage terms

are dominant. Despite the efforts to improve the energy balance closure, it is still an unsolved

problem which leads to a maximum closure, for the data collected in this work, of about 90%.

Another problem linked to the impossibility to perfectly close the energy balance is represented

by the difficult to match the footprint areas for the instruments which measure latent and sensible

heat fluxes, net radiation and ground heat flux. Latent and sensible heat fluxes have a

representative source area on the order of hundred meters, while for net radiometer it is equal to

about ten meters and for heat flux plate it is equal to about one meter.

Experimental campaigns to study the spatial scale of turbulent fluxes across bare and vegetated

soils have been performed in order to validate two analytical footprint models from literature.

These experiments have shown that the intra-field spatial distribution of latent, sensible and

carbon dioxide fluxes can be strongly differenced among them and, in bare soil, it is extremely

complicated to define a unique footprint model which accurately describes the representative

source area for the whole range of fluxes. Generally, in literature, footprint area is assumed to be

the same for the whole range of turbulent fluxes while, thanks to these experiments, it has been

possible to increase the knowledge about the latent, sensible heat and carbon dioxide spatial

variability which is the main feature analyzed in the footprint model.

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Acknowledges

This work was funded in the framework of the ACQWA EU/FP7 project (grant number 212250)

“Assessing Climate impacts on the Quantity and quality of WAter” , the framework of the

ACCA project funded by Regione Lombardia “Misura e modellazione matematica dei flussi di

ACqua e CArbonio negli agro-ecosistemi a mais” and PREGI (Previsione meteo idrologica per

la gestione irrigua) funded by Regione Lombardia.

The author thanks the University of Milan (Faculty of Agricultural and Food Sciences) for the

collaboration given in managing Landriano and Livraga eddy covariance stations.

Special thanks to Dr. Alessandro Ceppi, Ing. Chiara Corbari, Ing. Giovanni Ravazzani and Prof.

Marco Mancini for their help in setting up the experiments and their precious advices. Special

thanks also to the whole group of PhD students which are my colleagues and precious friends.