the noaa/faa/ncar winter precipitation test bed: how well are we measuring snow?
DESCRIPTION
The NOAA/FAA/NCAR Winter Precipitation Test Bed: How Well Are We Measuring Snow?. Roy Rasmussen 1 , Bruce Baker 2 , John Kochendorfer 2 , Tilden Myers 2 , Scott Landolt 1 , Alex Fisher 3 , Jenny Black 1 , Julie Theriault 1 , Paul Kucera 1 , David Gochis 1 , Craig Smith 3 , - PowerPoint PPT PresentationTRANSCRIPT
The NOAA/FAA/NCAR Winter Precipitation Test Bed:
How Well Are We Measuring Snow?
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Roy Rasmussen1, Bruce Baker2, John Kochendorfer2, Tilden Myers2, Scott Landolt1, Alex Fisher3, Jenny Black1,
Julie Theriault1, Paul Kucera1, David Gochis1, Craig Smith3, Rodica Nitu3,Mark Hall2,Steve Cristanelli1 and Ethan Gutmann1
1. National Center for Atmospheric Research (NCAR) 2. NOAA
3. Environment Canada
Winter Weather Nowcastingfor transportation requires real-time liquid equivalent measurements!
TT║║MESMESTT║║MESMES
ESSLJanuary
TT║║MESMESTT║║MESMES
ESSL
April
How will snowfall rates change in the future?
The NOAA/FAA/NCAR Winter Precipitation Test Bed was initially
established in 1991 at NCAR in Boulder, Colorado to address FAA
needs for real-time snowfall rates in support of ground deicing
The NOAA Climate Reference Network program started using the site in the late 90’s to evaluate snow measuring instrumentation for climate purposes.
Challenges of automatic snow fall rate measurements:
1. Wind under-catch - Gauge acting as obstacle to the flow, generating updrafts
2. Cap over of the orifice by snow accumulating on the gauge
3. Minimum detectable signal often large (to overcome noise)
4. Minimum detectable signal impacted by wind speed (higher the wind, the larger the minimum detectable signal)
5. Eliminating blowing snow false accumulations
6. High maintenance - Need to empty the bucket after snow fills up and refill bucket with
glycol and oil.
National Center for Atmospheric Research
Updraft generated upstream of gauge
Methods devised to solve the challenges:
1. Wind effect:- Wind shields used to prevent updrafts from forming over weighing gauges.
2. Orifice blocking effect- Heaters used to prevent snow build up on the body of the gauge.
3. Reduce minimum detectable signal by software and hardware:- Improved software to reduce false tips by vibration.- Improved hardware to eliminate vibrations and other noise.
4. Reduce the minimum detectable signals increase with wind speed- Use wind shields that have high efficiency (e.g. WMO Double
Fence Intercomparison Reference Shield)
Insert image of the Marshall site with DFIR
Deployed multiple Double Fence Inter-comparison Reference (DFIR) shields as “truth” gauge
Layout of site:
Flat and level site located 7 km south of Boulder, Colorado
NCAR owned and operated with security fence
11
Aerial View of the NOAA/FAA/NCAR Test site
13
View of test site to the South
15
View of test site towards the West
16
Developed and tested
double Alter shield
17
Developed and tested 2/3 DFIR
shield (CRN)
18
Developed and tested
hotplate snowgauge
19
Testing multiple hotplates
20
Documented snow under-
catch behavior of
various shields and
gauges
0
0.05
0.1
0.15
0.2
0.25
0.3
0.35
0.4
0
5
10
15
20
6 8 10 12 14 16
March 14, 2002
Original Hotplate Zeroed DFIR Zeroed NDblAlt Zeroed DblAlt Zeroed SngAlt Zeroed SmWyo Zeroed SmDFIR
10m Wind
Acc
umul
aton
(inc
hes) W
ind Speed (m
/s)
Time (Hrs)
Single Alter
Double Alter
Small DFIR
DFIRHotplate
Wind speed
21
Established transfer
functions for various shields
Established transfer
functions for various shields and
gauges0.2
0.4
0.6
0.8
1
1.2
-2 0 2 4 6 8
y = 0.96676 - 0.082568x R= 0.92561
y = 1.059 - 0.10492x R= 1
Orig
inal
hot
plat
e ac
cum
/DFI
R
accu
m (1
hou
r per
iods
)
10 m wind speed (m/s)
Single Alter Catch Efficiency
Hotplate Catch Efficiency
Data used to develop
transfer function shows
significant scatter!
24
Thank You!
Rasmussen et al. 2001
25
Mapped airflow around
shields/gauges using sonic
anemometers and numerical modeling
26
Established that visibility
is a poor method to
estimate the liquid
equivalent rate of snow
(light, moderate,
heavy)
NWS TABLE VISIBILITY (STATUE MILES) >0.50 >.25 -
<=.50 .25
Light Moderate Heavy
HVY
MOD
LGT
1.7 mm/hrModerate
28
Developed and tested the Liquid Water Equivalent system
for ground deicing use
Precipitation Type sensor (HSS)
WXT temperature, humidity, and wind sensor (Vaisala)
Hotplate (Yankee) Weighing Snowgauge
(GEONOR)
Snow Liquid WaterEquivalent System
Liquid Equivalent snowfall rate determination
Moderate Snow
Precipitation Type sensor (Vaisala PWD-22)
30
Developed method to heat the
orifice of a gauge using temperature controlled heat tape
(max temperature
2 ˚C)
31
Accurate snow depth measurements remain a
challenge!
32
Measured snow particle
size distribution using video disdrometer
Disdrometer Observations2DVD SpecificationsMeasurement area = 10
cm x 10 cmScan rate = 51.3 kHzHorizontal resolution =
0.15 mmVertical resolution = 0.03
mm for snowflakes, 0.1 mm for raindrops
Particle CharacteristicsHeight and widthVolumeTerminal velocity
Front view Side view
[mm] [mm]
~4 mm
Rain Period: 1230 (17 March)-0200 UTC (18 March)
2100-2400 UTC17 March
2225-2300 UTC17 March
Terminal Velocity vs Equ. Diameter
Hydrometeor Size Distribution
Mixed Phase Period: 0200-0630 UTC Decreasing temperature
0200-0600 UTC
0515-0520 UTC
Terminal Velocity vs Equ. Diameter
Hydrometeor Size Distribution
Partially-Melted Snow Period : 2020 UTC- Temperature >0oC; Temporal maximum temperature
2200-2300 UTC
2125-2130 UTC
Crystal Types:Irregulars (hvy) 1-2 mmSpatial dendrites /snow grains (hvy) <1-2 mmPlates (lgt-mod) <1-2 mmNeedles (mod) 2-4 mmStellars (mod) <1-2 mmAggregrate sizes 2-8 mm
Terminal Velocity vs Equ. Diameter
Hydrometeor Size Distribution
Snow Period: -2020 UTCTemperature slightly above 0oC; Small crystals
1100-1200 UTC
1950-1955 UTC
Crystal Type:Irregulars (hvy) 1-2 mmAggregrate sizes 3-4 mm
1900-2000 UTC
Terminal Velocity vs Equ. Diameter
Hydrometeor Size Distribution
38
Measured vertical
profile of precipitation
using K-band radar
39
Aircraft Deicing Fluid
testing
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Summary• The NOAA/FAA/NCAR Winter Precipitation Test Bed
has been used to investigate a number of important aspects of winter precipitation:
1. Under-catch of snow as a function of shield type and the development of transfer functions
2. Develop and test new wind shields3. Evaluate the use of various gauge/shield combinations
for both real-time and climate snow measurements. 4. Develop and test new precipitation instruments
(hotplate)5. Real-time measurement of snow for aircraft ground
deicing purposes6. The use of visibility to measure snow intensity7. Snow size distributions and terminal velocity8. Radar- reflectivity snowfall relationships
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SummaryHow well are we measuring snow?
• While advances in shields and gauges have been made, we still don’t fully understand the significant scatter in the data nor have we designed the perfect wind shield to reduce the scatter.
• Need to use direct measurements of the liquid equivalent rate of snow to estimate snow intensity in METARs rather than use visibility
• The automated measurement of precipitation type and snow depth remains a significant challenge.
42
Thank You!