baseline structural performance and aircraft impact damage

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Federal Building and Fire Safety Investigation of the World Trade Center Disaster Baseline Structural Performance and Aircraft Impact Damage Analysis September 14, 2005 Fahim Sadek Building and Fire Research Laboratory National Institute of Standards and Technology U.S. Department of Commerce [email protected]

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Page 1: Baseline Structural Performance and Aircraft Impact Damage

Federal Building and Fire Safety Investigation of the World Trade Center Disaster

Baseline Structural Performance and Aircraft Impact Damage Analysis

September 14, 2005

Fahim SadekBuilding and Fire Research LaboratoryNational Institute of Standards and Technology

U.S. Department of Commerce

[email protected]

Page 2: Baseline Structural Performance and Aircraft Impact Damage

DisclaimerDisclaimer

Certain commercial entities, equipment, products, or materials are identified in this document in order to describe a procedureor concept adequately or to trace the history of the procedures and practices used. Such identification is not intended to imply recommendation, endorsement, or implication that the entities, products, materials, or equipment are necessarily the best available for the purpose. Nor does such identification imply afinding of fault or negligence by the National Institute of Standards and Technology.

Page 3: Baseline Structural Performance and Aircraft Impact Damage

ContributorsContributors

• Contractors

A team of experts from Leslie E. Robertson Associates (LERA): development of the structural databases, reference structural models, and the baseline performance analysis of the WTC towers.

William J. FaschanLeslie E. Robertson Richard B. GarlockWilliam C. Howell Seung-Je Lee Raymond Lai Gayle Katzman

A team of experts from Skidmore, Owings, and Merrill (SOM): third-party review of the structural databases, reference models, baseline performance analysis, and the refined NIST estimate of the wind loads on the towers.

William F. BakerJohn J. ZilsRobert C. Sinn

Page 4: Baseline Structural Performance and Aircraft Impact Damage

ContributorsContributors• Contractors

A team of experts from Applied Research Associates (ARA): analysis of aircraft impacts into the WTC towers.

Steven W. KirkpatrickRobert T. BocchieriRobert A. MacNeillSamuel HolmesBrian D. PetersonRobert W. CilkeClaudia Navarro

Dr. David M. Parks: provided expertise in the area of computational mechanics for the aircraft impact analysis.

Page 5: Baseline Structural Performance and Aircraft Impact Damage

ContributorsContributors

• NISTDr. Emil Simiu: provided the wind engineering expertise required for the development of the wind loads on the WTC towers.

Dr. Michael A. Riley and Dr. William P. Fritz assisted with preliminary stability analyses of the towers. Dr. Fritz participated in the wind study.

Page 6: Baseline Structural Performance and Aircraft Impact Damage

Scope of ProjectScope of Project

• Baseline Performance

Develop reference structural models of the WTC towers.

Establish the baseline performance of the towers under design loading conditions (gravity and wind).

• Aircraft Impact Damage

Simulate aircraft impacts into the towers to estimate probable damage to structural, mechanical, and architectural systems; and establish the initial conditions for the fire dynamics modeling (Project 5) and thermal-structural response and collapse initiation analysis (Project 6).

Page 7: Baseline Structural Performance and Aircraft Impact Damage

Baseline Performance of the TowersBaseline Performance of the Towers

• Tasks

Develop structural databases of primary structural components for each of the two towers

Develop reference structural models of the WTC towers• Typical floor models

• Global models of the towers

Develop estimates of design wind loads on each of the two towersand evaluate current codes, standards, and practices

Establish baseline performance under wind and gravity loads• Demand/capacity ratios for components and connections

• Total and inter-story drifts (building sway under design wind loads)

Page 8: Baseline Structural Performance and Aircraft Impact Damage

Baseline Performance of the TowersBaseline Performance of the Towers

The baseline performance of the WTC towers under gravity and wind loads was established in order to assess the towers’ ability to withstand those loads safely, and to evaluate the reserve capacity of the towers to withstand unanticipated events such as a major fire or impact damage.

Wind loads were a governing factor in the design of the structural components that made up the frame-tube steel framing system. Wind load capacity is also a key factor in determining the overall strength of the towers and is important in evaluating:

• The baseline performance of the WTC towers

• The reserve capacity of the structures to withstand unanticipated events

• Design practices and procedures that were used

Accurate estimation of the wind load on tall buildings is a challenging task. The state of knowledge in wind engineering is evolving.

Page 9: Baseline Structural Performance and Aircraft Impact Damage

Structural DatabasesStructural Databases

StepsScanning and digitization of the original drawing booksA four-step quality control procedure

• First check during OCR process• Second check: random, but methodical check by an engineer• Third check: ‘cross-check rectify’

Programmatically compare with database developed by a consultant of the leaseholder of the towers

• Final review

Cross section property calculationsDevelopment of the relational databases, using Microsoft Access, to link the generated database files into a format suitable for the development of the structural global models

Page 10: Baseline Structural Performance and Aircraft Impact Damage

Structural DatabasesStructural Databases

• WTC DB Development: Modifications to DB

Modifications to Members of the WTC-DB

Item Summary Tower Element Floor Element Effected

WTC-DB Modified Archived

1 Core Column Reinforcing A and B Numerous 98-106

Core Columns Book 3 Book 19

2 Fiduciary Bank Vault B

Col. 508B and Col. 1008B 97-45

Core Columns Book 3

LERA P209

3

Bombing of 26 February 1993 - Repair A

Col. 324, Bracing G313A and G304A

B-2 Level

Perimeter Column and Bracing NA

LERA P1003118

4 EXCO Stair A Col. 901A 26 Core Column NA

LERA P1003249

Page 11: Baseline Structural Performance and Aircraft Impact Damage

Structural Databases ReviewStructural Databases Review

• Skidmore, Owings & Merrill (SOM) third-party reviewRandom checks of digitized databases and cross section propertiesResult:

• No discrepancies were found

• NIST In-house ReviewLine-by-line review of all filesRandom checks by project leaderCalculate all cross section properties and compare with LERA databaseResult:

• Minor discrepancies were identified between the LERA DB and the drawing bookso Examples: Book 1, entry 207 should be 287

Book 3, entry 3010 should be 301D• No discrepancies were found for cross section properties

Page 12: Baseline Structural Performance and Aircraft Impact Damage

Reference Structural ModelsReference Structural Models

• Task objective: Use structural databases to develop reference, finite element structural models of the towers. Models developed usingSAP2000 Version 8, and included:

Typical floor models

Global tower models

• Models were used:

to establish the baseline performance of the towers under design gravity and wind loads

as a reference for more detailed models used in the aircraft impact analysis (Project 2) and thermal-structural response and collapse initiation analysis (Project 6)

Page 13: Baseline Structural Performance and Aircraft Impact Damage

Reference Structural ModelsReference Structural ModelsFloor models:

3-D models of typical floor systems:• A truss floor system (96th floor of WTC 1)• A mechanical floor (75th floor of WTC 2)

Type 1 - WTC Typical Truss Floor Panel Plan

Tower A Floors: 10 - 24 60 - 66 Tower B Floors: 14 - 24 60 - 7426 - 40 68 - 74 26 - 40 84 - 9150 - 58 84 - 91 50 - 58 93 - 106

93 - 105Note: All panel types within 1" length tolerance, except floors 10,11, 39, 40, 70, & 71 which are within 6"-10". Floors 72-74 vary 18"-26".

FR1 ER1 DR1 CR1 BR1 A1 B1 C1 D1 E1 F1

Note: H1 = H6

Note: J1 =K1 = KR1

Note: HR1 = HR6 Note: H1 =M1 = MR1

(all C32T5 Trusses)

F1 E1 D1 C1 B1 A1 BR1 CR1 DR1 ER1 FR1

G1

G1

CORE

GR1

HI HR1

J1 J1

HR1 H1

GR1

Typical tenant Typical tenant floor systemsfloor systems

Page 14: Baseline Structural Performance and Aircraft Impact Damage

Floor Systems: Floor Systems: Floor 96Floor 96--AA ModelModel

Page 15: Baseline Structural Performance and Aircraft Impact Damage

Floor Systems: Floor Systems: Floor 75Floor 75--BB ModelModel

Page 16: Baseline Structural Performance and Aircraft Impact Damage

Global Tower ModelsGlobal Tower Models

3-D models of the 110-story structure and basement floors of each of the two towers

Models included:Core columns Exterior walls

• Foundation to floor 7• Trees (transition from 3’-4 to 10’-0 col. spacing)• Floor 9 to 106• Floor 107 to roof

Hat trussRigid floor diaphragmsFlexible floor diaphragms

Page 17: Baseline Structural Performance and Aircraft Impact Damage

Modeling of Exterior PanelsModeling of Exterior Panels

Equivalent beam model of exterior panel

Detailed shell model of an exterior panel

Page 18: Baseline Structural Performance and Aircraft Impact Damage

Modeling of Floor DiaphragmModeling of Floor Diaphragm

Equivalent floor diaphragm to capture the in-plane stiffness of the floor system

Page 19: Baseline Structural Performance and Aircraft Impact Damage

Global Tower Models: Below Floor 9Global Tower Models: Below Floor 9

Page 20: Baseline Structural Performance and Aircraft Impact Damage

Global Tower Models: Hat Truss Global Tower Models: Hat Truss

Page 21: Baseline Structural Performance and Aircraft Impact Damage

Reference Structural ModelsReference Structural Models

Model Number of

Joints Degrees of Freedom

Number of Frame Elements

Number of Shell Elements

Total Number of Elements

WTC 1 global model 53,700 218,700 73,900 10,000 83,900 WTC 2 global model 51,200 200,000 73,700 4,800 78,500 Typical truss-framed model 28,100 166,000 27,700 14,800 42,500 Typical beam-framed model 6,500 35,700 7,500 4,600 12,100

Page 22: Baseline Structural Performance and Aircraft Impact Damage

Structural Models Review and ValidationStructural Models Review and ValidationSOM Third-party Review

Consistency with original design• Random checks

Verification/validation of models• Review assumptions and level of detail• Perform analyses using various loading conditions to test the

accuracy of the models

NIST In-House ReviewConsistency with original design

• Models geometry / cross section properties• Material properties

Verification/validation of models• Review assumptions and level of detail• Perform analyses using various loading conditions to test the

accuracy of the modelsWorkshop for NIST investigators and contractors on October 28, 2003 to review the reference models

Page 23: Baseline Structural Performance and Aircraft Impact Damage

Review of Reference Structural ModelsReview of Reference Structural ModelsModeling assumptions and level of detail in the models were, in general, accurate and suitable for the purpose of the project.

Reviews indicated minor discrepancies between the developed reference models and the original design documents.

Identified two areas where the models needed to be modified:

• The effect of additional vertical stiffness of the exterior wall panels due to the presence of the spandrel beams

• Modeling of the connections of the floor slab to the exterior columns of the typical beam-framed floor model, where this connection appeared to be fixed while the connection should be modeled as pinned

The minor discrepancies and the areas identified for modification were reported to LERA who implemented the changes and modified the models accordingly.

The reference structural models were approved by NIST and made available for other phases of the NIST investigation.

Page 24: Baseline Structural Performance and Aircraft Impact Damage

Calculated frequencies and periods without PCalculated frequencies and periods without P--∆∆ effects for the WTCeffects for the WTC towers.towers.WTC 1 WTC 2

Frequency Period Frequency Period

(Hz) (s) (Hz) (s)

N–S 1 0.088 11.4 2 0.093 10.7

E–W 2 0.093 10.7 1 0.088 11.4

Torsion 3 0.192 5.2 3 0.192 5.2

N–S 4 0.233 4.3 5 0.263 3.8

E–W 5 0.263 3.8 4 0.238 4.2

Torsion 6 0.417 2.4 6 0.417 2.4

ModeMode

Direction of Motion

Calculated frequencies and periods with PCalculated frequencies and periods with P--∆∆ effects for the WTCeffects for the WTC towers.towers.WTC 1 WTC 2

Frequency Period Frequency Period

(Hz) (s) (Hz) (s)

N–S 1 0.083 12.1 2 0.089 11.2

E–W 2 0.088 11.3 1 0.083 12.1

Torsion 3 0.189 5.3 3 0.192 5.2

N–S 4 0.227 4.4 5 0.250 4

E–W 5 0.250 4 4 0.227 4.4

Torsion 8 0.455 2.2 8 0.455 2.2

ModeMode

Direction of Motion

Page 25: Baseline Structural Performance and Aircraft Impact Damage

Comparison of Measured and Calculated Natural Frequencies and Periods of WTC 1

N-S E-W Torsion N-S E-W Torsion

October 11, 1978 11.5 mph, E/SE 0.098 0.105 0.211 10.2 9.5 4.7

January 24, 1979 33 mph, E/SE 0.089 0.093 0.203 11.2 10.8 4.9

March 21, 1980 41 mph, E/SE 0.085 0.092 0.201 11.8 10.9 5.0

December 11, 1992 - 0.087 0.092 - 11.5 10.9 -

February 2, 19931 20 mph, NW 0.085 0.093 0.204 11.8 10.8 4.9March 13, 19931 32 mph, NW 0.085 0.094 0.199 11.8 10.6 5.0March 10, 19941 14 mph, W 0.094 0.094 0.196 10.6 10.6 5.1

December 25, 19942 N 0.081 0.091 - 12.3 11.0 -

Average - 0.088 0.094 0.202 11.4 10.6 4.9

Theoretical Value - 0.084 0.096 - 11.9 10.4 -

Reference Global ModelLERA/NIST - WTC 1

without P-Delta 0.088 0.093 0.192 11.4 10.7 5.2LERA/NIST - WTC 1

with P-Delta 0.083 0.088 0.189 12.1 11.3 5.3

Notes:1Reported frequency value is the average of the SW corner, NE corner, and center core frequency measurements.2Reported frequency is based on center core data only.

Orginal Design - Predicted Values

Direction of Motion

Frequency (HZ) Period (s)

Direction of MotionData Source/ Event Date Wind Speed &

Direction

Historical Data

Average of Measured Data

Page 26: Baseline Structural Performance and Aircraft Impact Damage

Natural Periods (s)Natural Periods (s)

WTC 1 AnalysisWTC 1 AnalysisN-S E-W Torsion

Average measured 11.4 10.6 4.9

Theoretical value (original design) 11.9 10.4 --

Reference global model 11.4 10.7 5.2(without P(without P--∆ ∆ effects)effects)

WTC 2 AnalysisWTC 2 AnalysisN-S E-W Torsion

Average measured -- -- --

Theoretical value (original design) 10.4 11.9 --

Reference global model 10.6 11.4 5.2(without P(without P--∆ ∆ effects)effects)

Page 27: Baseline Structural Performance and Aircraft Impact Damage

Wind LoadingWind Loading

Wind loads considered included:

Original WTC design wind loads, 1960’s

Wind loads based on two recent wind tunnel studies conducted by Cermak Peterka Peterson, Inc. (CPP) and Rowan Williams Davis and Irwin, Inc. (RWDI) for insurance litigation concerning the towers, 2002

Refined estimates of wind loads developed by NIST and reviewed by SOM, 2004

Page 28: Baseline Structural Performance and Aircraft Impact Damage

Comparison of Wind LoadsWind Load Estimates for WTC 1

Base Shear 103 kips Base Moment 106 kips-ft

N-S E-WMost

unfavorable combined

peak

About N-S

AboutE-W

Most unfavorable combined

peak

NYC Building Code 1938 5.3 5.3 4.2 4.2

NYC Building Code 1968 to date 9.3 9.3 7.7 7.7

RWDI / NYC Building Code 2002 11.4 10.5 13.0 10.1 10.5 12.2

RWDI / ASCE 7-98 2002 12.3 11.3 14.0 10.8 11.4 13.1

CPP / NYC Building Code 2002 NA NA NA NA NA NA

CPP / ASCE 7-98 2002 NA NA NA NA NA NA

NIST / third-party SOM review 2004 14.1 13.0 16.1 12.4 13.1 15.1

Original WTC Design 1960’s 9.8 10.6 14.0 10.3 9.1 13.7

Source Year

Page 29: Baseline Structural Performance and Aircraft Impact Damage

Comparison of Wind LoadsWind Load Estimates for WTC 2

Base Shear 103 kips Base Moment 106 kips-ft

N-S E-WMost

unfavorable combined

peak

About N-S

About E-W

Most unfavorable combined

peak

NYC Building Code 1938 5.3 5.3 4.2 4.2

NYC Building Code 1968 to date 9.3 9.3 7.6 7.6

RWDI / NYC Building Code 2002 9.7 11.1 12.3 10.1 9.2 11.3

RWDI / ASCE 7-98 2002 10.6 12.2 13.5 11.1 10.1 12.4

CPP / NYC Building Code 2002 NA NA NA NA NA NA

CPP / ASCE 7-98* 2002 15.1 15.3 17.1 15.5 14.0 17.0

NIST / third-party SOM review 2004 12.2 14.0 15.6 12.8 11.6 14.3

Original WTC Design 1960’s 13.1 10.1 16.5 8.8 12.6 15.2

Source Year

* Using ASCE 7-98 sections 6.5.4.1 and 6.6

Page 30: Baseline Structural Performance and Aircraft Impact Damage

Comparison of Wind LoadsComparison of Wind Loads

Base Shears and Base Moments Due to Wind Loads from Different Building Codes

1938NYC Code

1968-2001NYC Code

1964NY State Code

1965BOCA/BBC

1967Chicago

Municipal Code

Base Shear(103 kips) 5.3 9.3 9.5 9.8 8.7

Base Moment(106 kips-ft) 4.2 7.7 7.6 8.5 7.5

Page 31: Baseline Structural Performance and Aircraft Impact Damage

Comparison of Wind SpeedsComparison of Wind Speeds

Source Wind Speed (fastest-mile at 33 ft above ground over open terrain)

ASCE 7-02 88 mph

NYCBC 80 mph*

Original WTC design 67 – 75 mph

NIST estimate 96 mph

* This wind speed is assumed to be defined as a fastest-mile speed, even though no such definition is explicitly included in the NYCBC.

Page 32: Baseline Structural Performance and Aircraft Impact Damage

Refined NIST Estimates of Wind LoadsRefined NIST Estimates of Wind Loads

Task objective: to provide estimates of wind-induced forces and moments on the towers, based on considerations related to the state of the art in wind engineering.

NIST performed estimates of the wind effects on the WTC towers based on the limited information available at the time ofthe investigation. The information used included results of wind tunnel tests and extreme wind climatological estimates conducted by RWDI and CPP, wind speeds from the National Climatic Data Center, and the NIST hurricane wind speed database.

More elaborate calculations and/or test results would be desirable. However, obtaining such results was not practicable.

Page 33: Baseline Structural Performance and Aircraft Impact Damage

Refined NIST Estimates of Wind LoadsRefined NIST Estimates of Wind Loads

Summary Comparison by Weidlinger Associates, Inc., of CPP and RWDI Estimates

Approximate maximum base moments induced by ASCE 7-98 Standard wind loads for WTC 2

|My| (lb-ft) |Mx| (lb-ft) RWDI 2 (Table 2a) 10.1e+9 11.1e+9

CPP (Upper Table, p. 21) 14.0e+9 15.5e+9

Both RWDI and CPP results indicate that the critical base moments occur for an angle of about 210 degrees.

NIST estimates of wind-induced forces and moments had to rely primarily on RWDI results, since no results for WTC 1 are available from CPP. However, the estimates took into account a comparisonbetween RWDI and CPP results for WTC 2.

Page 34: Baseline Structural Performance and Aircraft Impact Damage

Refined NIST Estimates of Wind LoadsRefined NIST Estimates of Wind LoadsReview of CPP Estimates:

• NIST estimated a 720-yr, 3-s peak gust speed of 99.8 mph for 210°,while CPP’s estimate was 117.5 mph, i.e., CPP results overestimated wind loads by about 39% [(99.8/117.5)2 = 1/1.386].

• CPP results should be modified to account for their use of the sector-by-sector approach to integrate aerodynamic and extreme wind climatological data. This is not realistic physically and probabilistically.

• Using a rigorous probabilistic approach, NIST showed that CPP’s sector-by-sector approach underestimates wind effects with a specified mean recurrence interval. NIST preliminary estimates, that would need to be confirmed by research, indicate that the underestimation is about 15%.

• Therefore, the overall reduction factor applied to the estimated CPP effects to account for overestimated wind speed and underestimation resulting from the sector-by-sector approach should be approximately 20% (1.15/1.386≈1/1.205).

Page 35: Baseline Structural Performance and Aircraft Impact Damage

Refined NIST Estimates of Wind LoadsRefined NIST Estimates of Wind LoadsReview of RWDI Estimates:

• A comparison of RWDI results with the corrected CPP estimates indicates that the RWDI results underestimate the moments by about 15%.

• The underestimation is due largely to the assumption, inconsistent with published measurements, that wind profiles in hurricanes are flatter than in non-hurricane winds. Using this assumption, RWDI estimated the ratio between the responses to an 88 mph speed (ASCE 7-98) and an 80 mph speed (NYCBC) to be about 1.1, rather than about (88/80)2=1.21.

• Also, it is not clear that RWDI’s use of the out-crossing method (with hurricane wind speeds weighted in proportion to their squares) leads to unbiased estimates. No justification/references were provided for weighting procedure.

Page 36: Baseline Structural Performance and Aircraft Impact Damage

Sources of Major Differences in Wind Load Sources of Major Differences in Wind Load Estimation Methods Used in Current PracticeEstimation Methods Used in Current Practice

• Design wind speed (codes, standards, site-specific estimates)

• Hurricane wind profile (whether or not hurricane wind profiles are flatter than the profiles for extratropical windstorms)

• Estimation of “component” wind effects with a specified mean recurrence interval by integrating wind tunnel data with wind speed and direction information (e.g., up-crossing method, sector-by-sector method, storm passages approach)

• Estimation of “resultant” wind effects using load combination methods (e.g., principle of companion loads, companion point-in-time loads)

Page 37: Baseline Structural Performance and Aircraft Impact Damage

Refined NIST Estimates of Wind LoadsRefined NIST Estimates of Wind Loads

Summary

• Wind loads consistent with ASCE 7-02 Standard design wind speeds were estimated for both towers from RWDI results via multiplication by 1.15. This factor was recommended for baseline analysis. However, it may be that the actual number is anywhere between, say, 1.10 and 1.20.

Page 38: Baseline Structural Performance and Aircraft Impact Damage

Baseline Performance AnalysisBaseline Performance Analysis

• Load Combinations

Original WTC design loads case:• WTC design gravity (dead and live) loads

• Original WTC design wind loads.

Lower estimate, state-of-the-practice (SOP) case:• Current New York City Building Code (NYCBC) live loads

• RWDI wind loads with wind speed scaled to the current NYCBC wind speed (80 mph fastest mile).

Refined NIST estimate case:• Current ASCE 7 Standard (a national standard) live loads

• Refined wind loads developed by NIST based on considerations related to the current state of the art in wind engineering.

Page 39: Baseline Structural Performance and Aircraft Impact Damage

Calculation of DemandCalculation of Demand--toto--Capacity Ratios (Capacity Ratios (DCRsDCRs))

DCRs were estimated using the Allowable Stress Design (ASD) procedure as specified in the American Institute of Steel Construction (AISC) Specification for Structural Steel Buildings – Allowable Stress Design and Plastic Design.

Load Combinations:• Original WTC design loading case and the lower estimate

SOP case: AISC Specification (1989) and the NYCBC 2001.

• The refined NIST estimate case: ASCE 7-02 Standard.

Page 40: Baseline Structural Performance and Aircraft Impact Damage

DCRsDCRs for Exterior Walls of WTC 1 under Original for Exterior Walls of WTC 1 under Original Design CaseDesign Case

0 .00

0 .

50

0.75

1.

00

1 .08

North East South West

Page 41: Baseline Structural Performance and Aircraft Impact Damage

DCRsDCRs for Core Columns of WTC 1 under Original for Core Columns of WTC 1 under Original Design CaseDesign Case

601 602 603 604 605 606 607 608

106 FL 0.94 1.03 1.29 1.01 1.01 1.05 1.15 0.80105 FL 1.03 1.10 1.36 1.11 1.09 1.13 1.23 0.92104 FL 1.12 0.98 1.13 0.94 0.96 0.95 1.12 0.84103 FL 1.04 1.03 1.18 1.01 1.03 1.01 1.18 0.93102 FL 1.11 1.08 1.24 1.08 1.09 1.07 1.25 1.02101 FL 1.19 1.06 1.05 0.88 0.99 1.07 1.05 1.09100 FL 1.10 1.11 1.10 0.93 1.05 1.13 1.10 1.1899 FL 1.16 1.16 1.15 0.99 1.10 1.20 1.15 1.2798 FL 1.23 1.01 0.96 0.96 1.02 1.06 1.00 1.1897 FL 1.18 1.06 1.00 1.01 1.07 1.12 1.04 1.2596 FL 1.24 1.10 1.04 1.06 1.12 1.17 1.09 1.3395 FL 1.31 0.97 0.93 0.98 1.05 1.05 0.96 1.1294 FL 1.13 1.01 0.96 1.02 1.10 1.09 1.00 1.1893 FL 1.18 1.04 0.99 1.07 1.14 1.14 1.04 1.2492 FL 1.23 0.98 0.93 0.83 0.98 1.03 0.98 1.0791 FL 1.08 1.02 0.95 0.86 1.02 1.07 1.01 1.1290 FL 1.12 1.05 0.98 0.89 1.05 1.12 1.05 1.1789 FL 1.17 0.95 0.89 0.93 0.92 1.02 0.94 1.0388 FL 1.04 0.98 0.92 0.96 0.96 1.06 0.97 1.0887 FL 1.08 1.01 0.94 1.00 0.99 1.10 1.00 1.1286 FL 1.12 0.96 0.93 0.87 0.88 1.09 0.99 1.0085 FL 1.15 0.99 0.95 0.90 0.90 1.13 1.02 1.0484 FL 1.20 1.01 0.98 0.93 0.93 1.16 1.05 1.0883 FL 1.25 0.93 0.90 0.96 0.96 0.99 0.96 1.1182 FL 1.01 0.97 0.93 0.99 0.99 1.02 1.00 1.1681 FL 1.04 1.02 0.99 1.04 1.03 1.07 1.05 1.2180 FL 1.08 0.88 0.93 0.72 0.82 1.07 0.86 0.9779 FL 1.04 0.90 0.96 0.74 0.84 1.09 0.88 1.0178 FL 1.08 0.92 0.98 0.76 0.87 1.12 0.90 1.0577 FL 0.76 0.63 0.66 0.62 0.68 0.65 0.66 0.8576 FL 0.78 0.67 0.70 0.65 0.70 0.68 0.70 0.8675 FL 0.97 0.84 0.89 0.82 0.91 0.86 0.86 1.0074 FL 0.97 0.85 0.89 0.82 0.92 0.86 0.86 1.0173 FL 1.00 0.86 0.91 0.84 0.93 0.88 0.88 1.0472 FL 1.00 0.83 0.87 0.82 0.85 0.83 0.85 0.9971 FL 1.03 0.84 0.88 0.83 0.86 0.84 0.86 1.0270 FL 1.05 0.85 0.90 0.85 0.88 0.86 0.88 1.0469 FL 0.80 0.78 0.82 0.80 0.84 0.83 0.83 0.8668 FL 0.84 0.81 0.85 0.84 0.88 0.87 0.87 0.9167 FL 0.83 0.80 0.85 0.84 0.87 0.86 0.86 0.9066 FL 0.89 0.82 0.89 0.87 0.89 0.88 0.89 1.0765 FL 0.90 0.82 0.89 0.87 0.89 0.88 0.89 1.0964 FL 0.92 0.84 0.92 0.90 0.92 0.90 0.91 1.1263 FL 0.90 0.81 0.89 0.86 0.88 0.87 0.88 0.9962 FL 0.91 0.83 0.90 0.88 0.89 0.88 0.89 1.0161 FL 0.93 0.84 0.92 0.89 0.91 0.89 0.91 1.0360 FL 0.90 0.81 0.86 0.90 0.87 0.87 0.87 1.0559 FL 0.91 0.82 0.87 0.91 0.89 0.88 0.88 1.0758 FL 0.93 0.83 0.88 0.93 0.90 0.89 0.89 1.0957 FL 0.90 0.81 0.86 0.90 0.87 0.86 0.86 1.0556 FL 0.92 0.82 0.87 0.92 0.88 0.87 0.87 1.0755 FL 0.93 0.83 0.88 0.93 0.89 0.88 0.88 1.0854 FL 0.87 0.81 0.86 0.90 0.91 0.86 0.83 1.0453 FL 0.88 0.82 0.87 0.91 0.92 0.87 0.84 1.0652 FL 0.89 0.83 0.88 0.93 0.93 0.88 0.85 1.0851 FL 0.87 0.81 0.86 0.90 0.90 0.86 0.83 1.0450 FL 0.89 0.82 0.87 0.91 0.91 0.87 0.83 1.0549 FL 0.90 0.83 0.88 0.92 0.93 0.88 0.84 1.0748 FL 0.88 0.81 0.86 0.93 0.90 0.84 0.82 1.0347 FL 0.89 0.82 0.87 0.94 0.91 0.85 0.83 1.0546 FL 0.91 0.83 0.88 0.96 0.92 0.86 0.84 1.0745 FL 0.83 0.77 0.81 0.86 0.84 0.80 0.75 0.9244 FL 0.85 0.78 0.83 0.89 0.86 0.81 0.77 0.9543 FL 0.64 0.56 0.60 0.65 0.65 0.61 0.58 0.7042 FL 0.66 0.56 0.63 0.68 0.68 0.64 0.61 0.7241 FL 0.85 0.77 0.83 0.88 0.90 0.84 0.81 0.9240 FL 0.85 0.76 0.82 0.88 0.90 0.84 0.81 0.9239 FL 0.84 0.77 0.82 0.88 0.88 0.84 0.80 0.9038 FL 0.85 0.78 0.83 0.90 0.89 0.85 0.81 0.9137 FL 0.87 0.79 0.84 0.91 0.90 0.86 0.82 0.9336 FL 0.85 0.78 0.81 0.88 0.87 0.84 0.81 0.9135 FL 0.86 0.79 0.82 0.89 0.88 0.85 0.82 0.9234 FL 0.88 0.80 0.82 0.91 0.90 0.86 0.82 0.9333 FL 0.84 0.77 0.81 0.89 0.87 0.83 0.80 0.9232 FL 0.85 0.77 0.82 0.90 0.88 0.84 0.81 0.9331 FL 0.86 0.78 0.83 0.91 0.89 0.85 0.82 0.9430 FL 0.82 0.77 0.82 0.89 0.87 0.84 0.81 0.9229 FL 0.83 0.78 0.82 0.90 0.88 0.85 0.82 0.9428 FL 0.84 0.78 0.83 0.91 0.89 0.86 0.83 0.9527 FL 0.83 0.77 0.82 0.89 0.88 0.83 0.80 0.9326 FL 0.84 0.78 0.82 0.90 0.88 0.84 0.81 0.9425 FL 0.85 0.79 0.83 0.91 0.89 0.85 0.82 0.9524 FL 0.82 0.78 0.81 0.89 0.88 0.82 0.80 0.9423 FL 0.83 0.78 0.81 0.90 0.89 0.82 0.81 0.9522 FL 0.84 0.79 0.82 0.91 0.89 0.83 0.82 0.9621 FL 0.82 0.78 0.81 0.92 0.88 0.82 0.81 0.9420 FL 0.83 0.79 0.82 0.93 0.89 0.83 0.82 0.9619 FL 0.84 0.79 0.83 0.94 0.90 0.83 0.83 0.9718 FL 0.82 0.78 0.81 0.92 0.88 0.82 0.80 0.9317 FL 0.83 0.79 0.82 0.93 0.89 0.82 0.80 0.9416 FL 0.84 0.79 0.83 0.94 0.90 0.83 0.81 0.9515 FL 0.81 0.77 0.80 0.93 0.90 0.81 0.80 0.9314 FL 0.82 0.78 0.81 0.93 0.91 0.82 0.80 0.9413 FL 0.83 0.79 0.82 0.94 0.92 0.82 0.81 0.9512 FL 0.82 0.78 0.81 0.93 0.90 0.82 0.79 0.9411 FL 0.83 0.78 0.82 0.94 0.91 0.82 0.79 0.9510 FL 0.84 0.80 0.83 0.95 0.92 0.84 0.80 0.9609 FL 0.92 0.76 0.90 1.04 1.01 0.97 0.87 1.0308 FL 0.92 0.81 0.90 1.04 1.02 0.98 0.87 1.0407 FL 0.57 0.53 0.56 0.62 0.60 0.60 0.55 0.6106 FL 0.59 0.55 0.57 0.63 0.62 0.62 0.56 0.6205 FL 0.59 0.55 0.58 0.64 0.63 0.63 0.57 0.6204 FL 0.57 0.54 0.56 0.62 0.61 0.61 0.55 0.6003 FL 0.66 0.61 0.64 0.71 0.70 0.69 0.63 0.6902 FL 0.69 0.62 0.66 0.74 0.72 0.71 0.64 0.7201 FL 0.80 0.79 0.82 0.92 0.90 0.88 0.79 0.88B1 FL 0.79 0.78 0.81 0.91 0.89 0.87 0.79 0.88B2 FL 0.81 0.79 0.82 0.93 0.90 0.88 0.80 0.89B3 FL 0.77 0.75 0.81 0.89 0.87 0.87 0.78 0.84B4 FL 0.79 0.83 0.89 0.99 0.97 0.95 0.86 0.95B5 FL 0.80 0.83 0.90 1.00 0.98 0.96 0.87 0.96

LEVELTOWER A, DCR of CORE COLUMN

600's COLUMN NUMBER

0 .00

0 .

50

0.75

1.

00

1 .08

901 902 903 904 905 906 907 908

106 FL 0.76 0.98 0.97 0.80 0.85 1.10 1.02 0.76105 FL 0.82 1.05 1.02 0.71 0.91 1.16 1.08 0.80104 FL 0.83 0.95 0.94 1.13 0.75 0.96 0.97 0.80103 FL 0.92 1.01 0.98 1.21 0.80 1.01 1.02 0.89102 FL 1.01 1.07 1.03 0.89 0.88 1.05 1.07 0.97101 FL 0.87 0.96 0.86 0.98 0.78 0.89 0.98 0.84100 FL 0.94 1.01 0.88 1.04 0.84 0.93 1.03 0.9199 FL 1.01 1.05 0.91 1.10 0.90 0.97 1.08 0.9898 FL 1.02 0.92 0.81 0.99 0.88 0.90 0.94 1.0097 FL 1.09 0.96 0.83 1.05 0.93 0.93 0.98 1.0696 FL 1.16 1.00 0.86 1.10 0.99 0.97 1.02 1.1395 FL 0.91 0.84 0.81 0.88 0.86 0.86 0.90 1.0894 FL 0.96 0.88 0.83 0.92 0.91 0.89 0.94 1.1493 FL 1.00 0.91 0.85 0.96 0.95 0.92 0.97 1.2092 FL 0.89 0.86 0.78 0.90 0.90 0.86 0.87 1.0491 FL 0.93 0.89 0.80 0.94 0.94 0.89 0.90 1.0990 FL 0.97 0.92 0.82 0.98 0.98 0.92 0.93 1.1489 FL 1.01 0.84 0.76 0.84 0.84 0.83 0.85 1.0088 FL 1.05 0.86 0.78 0.87 0.88 0.85 0.88 1.0587 FL 1.09 0.89 0.80 0.90 0.91 0.88 0.90 1.0986 FL 0.97 0.85 0.75 0.93 0.78 0.87 0.86 0.9785 FL 1.01 0.87 0.77 0.96 0.81 0.89 0.88 1.0084 FL 1.04 0.90 0.79 0.99 0.83 0.92 0.91 1.0483 FL 1.07 0.79 0.73 0.86 0.79 0.87 0.80 1.0782 FL 1.11 0.81 0.75 0.89 0.82 0.89 0.82 1.1181 FL 1.15 0.83 0.77 0.92 0.84 0.91 0.84 1.1480 FL 1.19 0.86 0.85 0.95 0.87 0.94 0.86 1.1979 FL 1.25 0.89 0.88 0.99 0.91 0.97 0.89 1.2478 FL 1.30 0.92 0.90 1.03 0.94 1.00 0.92 1.3077 FL 0.84 0.67 0.62 0.71 0.60 0.56 0.55 0.8876 FL 0.85 0.71 0.65 0.73 0.63 0.60 0.60 0.9075 FL 0.98 0.85 0.84 0.94 0.76 0.85 0.88 1.0574 FL 0.98 0.85 0.84 0.95 0.77 0.85 0.88 1.0673 FL 1.01 0.87 0.86 0.97 0.79 0.87 0.90 1.0972 FL 0.95 0.89 0.79 0.92 0.77 0.82 0.85 1.0371 FL 0.98 0.91 0.81 0.94 0.79 0.85 0.87 1.0670 FL 1.00 0.93 0.82 0.96 0.81 0.87 0.88 1.0869 FL 0.81 0.81 0.79 0.91 0.77 0.82 0.84 0.8868 FL 0.88 0.87 0.82 0.96 0.82 0.88 0.89 0.9567 FL 0.86 0.85 0.82 0.96 0.81 0.86 0.87 0.9266 FL 1.01 0.93 0.85 0.98 0.83 0.88 0.89 1.0965 FL 1.03 0.93 0.85 0.98 0.83 0.89 0.89 1.1164 FL 1.06 0.97 0.88 1.02 0.87 0.92 0.92 1.1463 FL 1.00 0.91 0.83 0.97 0.82 0.94 0.88 1.0762 FL 1.03 0.93 0.84 0.99 0.84 0.96 0.89 1.1061 FL 1.05 0.95 0.85 1.01 0.85 0.99 0.91 1.1260 FL 0.99 0.90 0.83 0.97 0.83 0.93 0.87 1.0659 FL 1.01 0.92 0.84 0.99 0.85 0.95 0.88 1.0858 FL 1.03 0.93 0.86 1.01 0.87 0.97 0.90 1.1057 FL 1.06 0.88 0.84 1.01 0.85 0.93 0.84 1.0456 FL 1.08 0.90 0.85 1.02 0.86 0.94 0.85 1.0655 FL 1.10 0.91 0.86 1.04 0.88 0.96 0.87 1.0954 FL 1.04 0.93 0.84 1.01 0.86 0.91 0.88 1.1153 FL 1.06 0.94 0.85 1.02 0.87 0.93 0.89 1.1352 FL 1.08 0.96 0.87 1.04 0.89 0.95 0.91 1.1551 FL 1.03 0.89 0.85 0.99 0.86 0.97 0.83 1.0950 FL 1.05 0.90 0.86 1.01 0.87 0.98 0.85 1.1149 FL 1.07 0.91 0.87 1.03 0.89 1.00 0.86 1.1348 FL 1.09 0.83 0.83 0.97 0.86 0.89 0.83 1.0847 FL 1.12 0.85 0.85 0.98 0.87 0.92 0.85 1.1146 FL 1.14 0.87 0.86 1.00 0.89 0.93 0.87 1.1345 FL 0.85 0.78 0.77 0.76 0.83 0.84 0.79 0.8844 FL 0.87 0.80 0.79 0.78 0.85 0.86 0.81 0.9043 FL 0.75 0.61 0.60 0.69 0.63 0.66 0.62 0.7742 FL 0.77 0.63 0.63 0.72 0.66 0.68 0.64 0.7941 FL 1.00 0.85 0.83 0.94 0.86 0.90 0.86 1.0040 FL 1.00 0.85 0.83 0.94 0.85 0.90 0.86 1.0039 FL 0.98 0.83 0.84 0.94 0.84 0.89 0.84 1.0138 FL 1.00 0.84 0.85 0.96 0.85 0.90 0.85 1.0237 FL 1.01 0.85 0.86 0.97 0.86 0.92 0.86 1.0436 FL 1.02 0.84 0.85 0.95 0.84 0.90 0.85 1.0135 FL 1.03 0.85 0.86 0.96 0.85 0.91 0.86 1.0334 FL 1.05 0.86 0.87 0.97 0.87 0.92 0.87 1.0433 FL 1.02 0.84 0.85 0.94 0.84 0.90 0.85 1.0232 FL 1.04 0.85 0.87 0.96 0.85 0.91 0.86 1.0331 FL 1.05 0.86 0.88 0.97 0.86 0.92 0.87 1.0430 FL 1.04 0.85 0.86 0.94 0.83 0.91 0.86 1.0229 FL 1.05 0.86 0.87 0.95 0.84 0.92 0.87 1.0328 FL 1.06 0.87 0.89 0.96 0.85 0.93 0.88 1.0427 FL 1.17 0.86 0.87 0.97 0.84 0.91 0.86 1.0226 FL 1.18 0.87 0.88 0.98 0.85 0.92 0.87 1.0325 FL 1.07 0.88 0.89 0.99 0.86 0.93 0.88 1.0524 FL 1.05 0.86 0.88 0.97 0.85 0.91 0.85 1.0323 FL 1.06 0.87 0.89 0.98 0.86 0.92 0.86 1.0422 FL 1.07 0.88 0.90 0.99 0.87 0.93 0.87 1.0521 FL 1.05 0.87 0.89 0.97 0.86 0.92 0.86 1.0620 FL 1.07 0.88 0.90 0.98 0.87 0.93 0.87 1.0719 FL 1.08 0.89 0.91 0.99 0.87 0.94 0.88 1.0918 FL 1.08 0.87 0.88 0.96 0.87 0.92 0.87 1.0617 FL 1.10 0.88 0.89 0.97 0.88 0.93 0.88 1.0816 FL 1.11 0.89 0.90 0.98 0.89 0.94 0.89 1.0915 FL 1.09 0.86 0.89 0.99 0.86 0.93 0.87 1.0814 FL 1.10 0.87 0.90 1.00 0.87 0.94 0.88 1.0913 FL 1.11 0.88 0.91 1.01 0.88 0.95 0.89 1.1012 FL 1.09 0.87 0.90 0.98 0.86 0.94 0.87 1.0811 FL 1.11 0.88 0.91 0.99 0.87 0.95 0.88 1.0910 FL 1.13 0.89 0.93 1.01 0.89 0.96 0.89 1.1109 FL 0.91 0.86 0.89 0.97 0.99 1.03 0.97 1.0608 FL 0.98 0.91 0.95 1.03 1.00 1.04 0.97 1.0607 FL 0.63 0.60 0.61 0.62 0.67 0.59 0.59 0.6206 FL 0.65 0.62 0.63 0.64 0.69 0.61 0.60 0.6405 FL 0.65 0.63 0.64 0.65 0.70 0.62 0.61 0.6404 FL 0.63 0.61 0.62 0.63 0.67 0.60 0.59 0.6203 FL 0.72 0.69 0.71 0.72 0.80 0.68 0.67 0.7102 FL 0.75 0.71 0.73 0.74 0.83 0.70 0.69 0.7401 FL 1.07 0.89 0.92 1.01 1.00 0.96 0.90 1.07B1 FL 1.06 0.88 0.91 1.00 0.98 0.94 0.88 1.06B2 FL 1.08 0.89 0.92 1.01 0.99 0.96 0.90 1.08B3 FL 1.02 0.85 0.89 0.97 0.93 0.92 0.86 1.01B4 FL 1.05 0.87 0.98 1.07 1.05 1.00 0.94 1.13B5 FL 1.06 0.88 0.99 1.08 1.06 1.01 0.95 1.14

LEVELTOWER A, DCR of CORE COLUMN

900's COLUMN NUMBER

1001 1002 1003 1004 1005 1006 1007 1008

106 FL 0.93 1.12 1.07 0.82 0.95 1.23 1.02 0.96105 FL 0.99 0.84 1.13 0.91 1.01 0.94 1.11 1.03104 FL 0.87 1.07 1.01 0.84 0.90 1.10 1.03 0.90103 FL 0.93 1.15 1.07 0.91 0.95 1.18 1.10 0.95102 FL 1.00 1.00 1.12 0.98 1.00 1.25 0.97 1.01101 FL 0.83 1.00 0.93 0.85 0.89 1.03 0.97 0.83100 FL 0.88 1.06 0.98 0.91 0.93 1.08 1.02 0.8999 FL 0.93 1.12 1.02 0.96 0.97 1.14 1.08 0.9498 FL 0.74 0.84 0.89 0.90 0.88 0.78 0.91 0.7497 FL 0.78 0.89 0.93 0.95 0.92 0.82 0.95 0.7896 FL 0.82 0.93 0.97 1.00 0.96 0.86 1.00 0.8295 FL 0.66 0.82 0.75 0.87 0.85 0.76 0.83 0.6694 FL 0.69 0.86 0.77 0.91 0.88 0.79 0.87 0.7093 FL 0.72 0.89 0.80 0.95 0.91 0.82 0.90 0.7392 FL 0.69 0.79 0.72 0.91 0.78 0.74 0.80 0.6991 FL 0.71 0.82 0.75 0.95 0.80 0.77 0.83 0.7290 FL 0.74 0.85 0.77 0.98 0.83 0.80 0.86 0.7489 FL 0.81 0.77 0.66 0.86 0.78 0.70 0.77 0.8188 FL 0.84 0.79 0.68 0.89 0.80 0.73 0.80 0.8487 FL 0.87 0.82 0.70 0.92 0.83 0.75 0.83 0.8786 FL 0.82 0.92 0.76 0.91 0.78 0.81 0.93 0.8285 FL 0.85 0.95 0.78 0.94 0.81 0.84 0.96 0.8584 FL 0.87 0.98 0.80 0.97 0.83 0.86 0.99 0.8883 FL 0.90 0.92 0.74 0.92 0.77 0.81 0.93 0.9082 FL 0.93 0.95 0.76 0.94 0.79 0.83 0.96 0.9381 FL 0.96 0.97 0.78 0.97 0.81 0.86 0.98 0.9680 FL 0.91 1.01 0.70 1.00 0.87 0.88 1.02 0.9179 FL 0.94 1.04 0.72 1.03 0.89 0.92 1.05 0.9478 FL 0.98 1.09 0.75 1.08 0.92 0.95 1.10 0.9877 FL 0.66 0.73 0.65 0.71 0.67 0.68 0.73 0.6776 FL 0.68 0.74 0.67 0.70 0.72 0.70 0.75 0.6875 FL 0.88 0.91 0.86 0.93 0.93 0.89 0.92 0.8974 FL 0.89 0.92 0.86 0.95 0.94 0.90 0.93 0.9073 FL 0.91 0.94 0.88 0.97 0.95 0.92 0.96 0.9272 FL 0.87 0.89 0.84 0.91 0.89 0.87 0.91 0.8771 FL 0.89 0.91 0.85 0.94 0.91 0.89 0.93 0.8970 FL 0.91 0.93 0.87 0.96 0.93 0.91 0.95 0.9169 FL 0.84 0.87 0.84 0.92 0.88 0.84 0.88 0.8468 FL 0.87 0.90 0.87 0.96 0.91 0.87 0.92 0.8767 FL 0.87 0.91 0.87 0.96 0.91 0.88 0.92 0.8866 FL 0.91 0.93 0.86 0.99 0.95 0.90 0.95 0.9165 FL 0.92 0.95 0.87 1.01 0.96 0.92 0.96 0.9364 FL 0.94 0.97 0.89 1.03 0.98 0.94 0.98 0.9463 FL 0.91 0.93 0.85 1.01 0.95 0.89 0.93 0.9162 FL 0.93 0.95 0.86 1.03 0.96 0.91 0.95 0.9361 FL 0.94 0.97 0.88 1.05 0.98 0.92 0.97 0.9560 FL 0.91 0.93 0.83 1.01 0.94 0.89 0.93 0.9159 FL 0.92 0.94 0.84 1.03 0.95 0.91 0.95 0.9258 FL 0.94 0.96 0.86 1.05 0.97 0.92 0.97 0.9457 FL 0.92 0.93 0.83 1.02 0.94 0.89 0.93 0.9256 FL 0.93 0.94 0.84 1.04 0.95 0.90 0.95 0.9355 FL 0.95 0.96 0.85 1.05 0.97 0.92 0.97 0.9554 FL 0.89 0.93 0.82 1.03 0.94 0.89 0.93 0.8953 FL 0.91 0.94 0.83 1.04 0.95 0.90 0.95 0.9152 FL 0.92 0.96 0.84 1.06 0.96 0.91 0.96 0.9251 FL 0.90 0.93 0.82 1.00 0.93 0.88 0.93 0.9150 FL 0.92 0.94 0.83 1.02 0.95 0.89 0.95 0.9249 FL 0.93 0.95 0.84 1.04 0.96 0.91 0.96 0.9348 FL 0.89 0.90 0.80 1.01 0.90 0.85 0.89 0.8947 FL 0.90 0.92 0.81 1.03 0.91 0.86 0.90 0.9046 FL 0.91 0.93 0.82 1.05 0.93 0.87 0.92 0.9145 FL 0.83 0.84 0.74 0.96 0.86 0.79 0.82 0.8344 FL 0.85 0.86 0.76 0.99 0.88 0.81 0.84 0.8543 FL 0.66 0.65 0.59 0.74 0.68 0.62 0.64 0.6642 FL 0.68 0.66 0.60 0.75 0.70 0.63 0.65 0.6841 FL 0.89 0.88 0.80 0.97 0.88 0.83 0.87 0.8940 FL 0.89 0.88 0.80 0.98 0.89 0.83 0.88 0.9039 FL 0.88 0.87 0.81 0.99 0.87 0.83 0.86 0.8938 FL 0.89 0.88 0.82 1.01 0.88 0.84 0.87 0.9037 FL 0.91 0.89 0.83 1.02 0.89 0.85 0.88 0.9136 FL 0.89 0.87 0.81 0.97 0.87 0.83 0.85 0.9035 FL 0.91 0.88 0.82 0.99 0.87 0.84 0.86 0.9134 FL 0.92 0.89 0.83 1.00 0.88 0.85 0.88 0.9233 FL 0.88 0.87 0.81 0.98 0.85 0.84 0.86 0.8932 FL 0.89 0.88 0.82 1.00 0.86 0.85 0.87 0.9031 FL 0.91 0.89 0.83 1.01 0.87 0.86 0.88 0.9130 FL 0.90 0.85 0.79 0.99 0.85 0.84 0.84 0.9029 FL 0.91 0.86 0.80 1.01 0.86 0.85 0.85 0.9128 FL 0.92 0.87 0.81 1.02 0.87 0.86 0.86 0.9227 FL 0.89 0.85 0.80 1.00 0.85 0.84 0.84 0.8926 FL 0.90 0.86 0.81 1.01 0.86 0.85 0.85 0.9025 FL 0.91 0.87 0.82 1.02 0.87 0.86 0.86 0.9124 FL 0.88 0.85 0.80 0.99 0.85 0.84 0.84 0.8823 FL 0.89 0.86 0.81 1.00 0.86 0.85 0.85 0.8922 FL 0.90 0.87 0.82 1.01 0.87 0.86 0.86 0.9021 FL 0.88 0.85 0.81 1.00 0.85 0.84 0.84 0.8820 FL 0.89 0.86 0.81 1.01 0.86 0.85 0.85 0.8919 FL 0.89 0.87 0.82 1.02 0.86 0.86 0.86 0.9018 FL 0.87 0.85 0.81 1.01 0.84 0.83 0.84 0.8717 FL 0.88 0.86 0.82 1.02 0.84 0.84 0.85 0.8816 FL 0.89 0.87 0.83 1.03 0.85 0.85 0.86 0.8915 FL 0.87 0.85 0.81 1.00 0.84 0.83 0.85 0.8714 FL 0.88 0.86 0.82 1.01 0.85 0.84 0.85 0.8813 FL 0.89 0.87 0.83 1.02 0.85 0.85 0.86 0.8912 FL 0.88 0.85 0.82 1.01 0.84 0.84 0.85 0.8811 FL 0.89 0.86 0.82 1.02 0.85 0.85 0.86 0.8910 FL 0.90 0.87 0.84 1.04 0.86 0.86 0.87 0.9009 FL 0.96 0.84 0.81 0.98 0.80 0.84 0.90 0.8908 FL 0.96 0.87 0.85 1.03 0.83 0.87 0.91 0.9307 FL 0.79 0.73 0.73 0.87 0.73 0.74 0.75 0.7906 FL 0.80 0.74 0.74 0.88 0.74 0.76 0.76 0.8105 FL 0.81 0.75 0.75 0.89 0.74 0.76 0.77 0.8104 FL 0.79 0.73 0.73 0.86 0.73 0.74 0.75 0.7903 FL 0.86 0.79 0.79 0.94 0.78 0.80 0.81 0.8602 FL 0.88 0.80 0.80 0.96 0.79 0.81 0.82 0.8801 FL 0.84 0.83 0.79 0.95 0.83 0.81 0.83 0.84B1 FL 0.83 0.82 0.78 0.94 0.83 0.80 0.82 0.83B2 FL 0.84 0.83 0.79 0.95 0.84 0.81 0.83 0.84B3 FL 0.86 0.82 0.79 0.92 0.81 0.82 0.80 0.87B4 FL 0.92 0.83 0.85 0.99 0.86 0.83 0.86 0.88B5 FL 0.93 0.83 0.85 1.00 0.86 0.83 0.86 0.88

LEVELTOWER A, DCR of CORE COLUMN

1000's COLUMN NUMBER

Line 600 Line 900 Line 1000

Page 42: Baseline Structural Performance and Aircraft Impact Damage

Results of Baseline Analysis for WTC 1Results of Baseline Analysis for WTC 1

* Number of members includes columns with ½ floor height due to the presence of column splices.The safety of the WTC towers on September 11, 2001 was most likely not affected by the fraction of members for which the demand exceeded allowable capacity.

Mean DCR

% members with DCR>1

% members with DCR>1.05

Approx. # of members with

DCR>1.05

Max DCR

Exterior Columns (Floor 9-106)Original WTC Design LoadsLower Estimate SOP CaseRefined NIST Estimate Case

0.760.781.10

1.1272

0.40.960

121*

281*

18,572*

1.311.442.05

Spandrel Beams (Floor 9-106)Original WTC Design LoadsLower Estimate SOP CaseRefined NIST Estimate Case

0.310.320.52

00

0.5

00

0.3

00

109

0.830.801.32

Core ColumnsOriginal WTC Design LoadsLower Estimate SOP CaseRefined NIST Estimate Case

0.860.860.84

109.98.9

5.35.35.2

278278270

1.361.361.40

Hat Truss (Columns)Original WTC Design LoadsLower Estimate SOP CaseRefined NIST Estimate Case

0.470.450.53

0.40.43.8

0.40.40.8

112

1.261.261.26

Page 43: Baseline Structural Performance and Aircraft Impact Damage

Results of Drift AnalysisResults of Drift AnalysisWTC 1 WTC 2

E–W N–S E–W N–STotal Drift (in.)

Drift Ratio

Total Drift (in.)

Drift Ratio

Total Drift (in.)

Drift Ratio

Total Drift (in.)

Drift Ratio

Original design case 56.6 H/304 55.7 H/309 51.2 H/335 65.3 H/263

SOP case 56.8 H/303 68.1 H/253 59.7 H/287 56.1 H/306Refined NIST case 70.6 H/244 83.9 H/205 75.6 H/227 71.0 H/242

Loading Case

0

200

400

600

800

1000

1200

1400

1600

0 20 40 60 80 100

Cumulative Drift [in.]

Hei

ght a

bove

B6

Leve

l [ft

.]

Drift MAX=56.6

E–W direction

0

200

400

600

800

1000

1200

1400

1600

0 20 40 60 80 100

Cumulative Drift [in.]H

eigh

t abo

ve B

6 Le

vel [

ft.]

Drift MAX=55.7

N–S direction

Cumulative drifts for WTC 1 under original design wind loads

Typical drift values considered in practice (not required by building codes) range from H/400 to H/500.

Page 44: Baseline Structural Performance and Aircraft Impact Damage

Results of Drift AnalysisResults of Drift AnalysisCurrent building codes do not specify a drift limit for wind design. The ASCE 7-02 Standard states in Section B.1.2 that the drift of structures due to wind effects shall not impair the serviceability of the structure. The commentary to this section indicates that drift limits in common usage for building design are on the order of 1/400 to 1/600 of the building height to minimize damage to cladding and nonstructural walls and partitions.

Structural engineers often use in their practice the criterion that total drift ratios should not exceed H/400 to H/500 for serviceabilityconsiderations and to enhance overall safety and stability (including P-∆ effects).

Limiting total building drift under wind loads was not part of the original design. Instead, inter-story drifts were used during the design stage for serviceability considerations.

Page 45: Baseline Structural Performance and Aircraft Impact Damage

Maximum Inter-story drift for WTC 1 and WTC 2WTC 1 WTC 2

E–W N–S E–W N–S

Original design case h/225 h/230 h/230 h/195

SOP case h/225 h/185 h/200 h/215

Refined NIST case h/180 h/150 h/160 h/175

Loading Case

0

200

400

600

800

1000

1200

1400

1600

0.00 0.20 0.40 0.60

Interstory Drift/Story Height [%]

Hei

ght a

bove

B6

Leve

l [ft

.]

E–W direction 0

200

400

600

800

1000

1200

1400

1600

0.00 0.20 0.40 0.60

Interstory Drift/Story Height [%]

Hei

ght a

bove

B6

Leve

l [ft

.]N–S direction

Inter-story drifts for WTC 1 under original design wind loads

Typical inter-story drift values considered in practice for serviceability (not required by building codes) range from h/300 to h/400.

Page 46: Baseline Structural Performance and Aircraft Impact Damage

Performance of Exterior wall columnsPerformance of Exterior wall columns

Distribution of normal stresses in the exterior walls at floor 39 of WTC 1 due to original wind loads only

Behavior of the super-structure is that of a framed tube system.

Stresses in ksi

Page 47: Baseline Structural Performance and Aircraft Impact Damage

Performance of Exterior wall columnsPerformance of Exterior wall columns

Distribution of normal stresses in the exterior walls at floor B-6 of WTC 1 due to original wind loads only

Behavior of the lower portion of the tower at the basement floors resembled that of a braced frame.

Stresses in ksi

Page 48: Baseline Structural Performance and Aircraft Impact Damage

Tensile Forces in Exterior Wall Columns under Tensile Forces in Exterior Wall Columns under Original Dead and Wind LoadsOriginal Dead and Wind Loads

kips

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 2 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 6 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 13 3 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

2 18 6 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 23 11 4 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

3 25 15 8 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 2

0 30 19 12 4 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 4

4 33 23 16 9 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 8

0 41 28 21 15 5 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 4 12

5 44 31 25 19 11 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 8 18

0 52 35 30 24 16 6 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 4 11 22

6 53 39 35 30 22 12 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 9 15 27

0 61 43 40 34 29 18 7 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 5 1 2 17 28

9 64 46 45 40 35 25 12 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 3 10 1 6 20 37

0 79 55 53 48 43 32 19 5 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 9 17 2 2 27 45

16 98 61 58 55 51 40 26 11 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 5 15 21 2 7 33 75

0 113 79 73 66 55 40 25 9 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 5 19 31 4 0 47 67

0 111 77 72 64 53 38 23 6 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 3 17 29 3 8 46 65

20 111 93 86 72 58 40 23 5 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 3 21 38 5 4 65 73

0 142 96 91 77 66 49 30 11 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 28 42 5 6 63 93

17 139 99 96 84 73 56 37 20 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 6 34 47 6 1 67 104

0 150 105 102 91 79 63 44 26 6 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 5 2 3 40 53 6 5 71 100

18 146 106 106 97 87 70 53 33 12 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 12 2 9 46 58 6 9 75 109

0 160 113 112 103 94 76 59 40 20 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 17 3 4 52 64 7 4 77 108

19 157 120 117 110 100 83 66 46 26 4 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 4 23 4 0 57 69 7 9 85 119

0 172 129 122 115 107 91 74 52 32 9 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 10 30 4 7 64 74 8 2 90 118

21 170 133 128 123 114 99 79 60 39 16 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 16 35 5 3 69 80 8 8 96 132

0 188 141 136 131 120 106 86 67 44 21 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 21 40 5 9 75 87 9 4 99 131

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0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

1.28 12.86 5. 05 0.40 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 17.55 7. 57 2.66 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 07 0 .00

2.33 19.66 10.25 5.65 1.02 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 2. 25 0 .00

0.00 24.24 13.94 9.26 4.59 0. 06 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 1.34 5. 16 0 .00

3.61 26.39 17.26 12. 33 7.05 2. 30 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .19 4.31 8. 62 0 .00

0.00 35.66 21.20 16. 45 11.11 5. 76 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 3 .41 8.12 12.24 0 .00

7.26 41.85 25.80 21. 07 15.92 9. 90 2.86 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 2.2 0 8 .17 1 3.21 17.89 0 .00

0.00 65.75 31.08 24. 85 19.00 12.32 5.21 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 4.6 5 10. 90 1 6.74 22.69 0 .00

22. 25 60.71 38.93 32. 60 25.12 17.88 10. 80 4.03 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 4.05 10.98 18. 18 2 5.63 32.18 0 .00

20. 90 59.12 37.77 31. 39 23.92 16.68 9.59 2.72 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 2.85 9.7 7 16. 98 2 4.43 31.02 0 .00

0.00 71.10 49.32 40. 23 30.92 23.84 15. 94 7.71 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .89 9.24 17.06 24. 11 3 2.41 39.87 0 .00

9.72 82.65 51.49 42. 70 34.00 28.24 19. 44 10.68 1. 45 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 3 .85 12. 41 20.88 26. 82 3 5.20 44.34 0 .00

0.00 91.89 55.85 46. 93 38.20 31.98 22. 55 13.37 4. 61 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 6 .53 15. 42 24.48 30. 91 3 9.23 47.76 0 .00

12. 07 88.86 59.46 51. 31 42.97 35.46 25. 92 16.45 7. 09 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.5 2 9 .55 18. 64 27.78 35. 38 4 3.82 52.67 0 .00

0.00 98.00 64.87 55. 20 46.32 38.26 29. 11 19.74 9. 94 0.73 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 3.3 8 12. 87 21. 95 30.84 38. 68 4 6.96 55.18 0 .00

13. 58 96.21 67.41 58. 68 49.84 40.92 31. 78 22.36 13.18 4.12 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 6.6 5 15. 49 24. 55 33.36 41. 96 5 0.56 59.27 0 .00

0.00 108.19 72.10 62. 72 53.49 43.96 35. 01 25.80 16.26 7.16 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.66 9.6 9 18. 89 27. 84 36.53 45. 63 5 4.01 61.71 0 .00

14. 51 107.78 73.55 65. 48 56.53 47.47 39. 03 29.82 19.74 10. 88 1.30 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 4.25 13.09 22. 76 31. 67 39.87 48. 49 5 7.24 65.84 0 .00

0.00 120.62 78.36 69. 41 60.22 50.51 42. 56 32.78 23.21 14. 65 5.14 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 7.93 16.53 25. 71 35. 17 43.04 52. 27 6 0.78 68.44 0 .00

16. 41 118.82 80.57 73. 80 64.95 54.32 46. 76 36.78 26.65 17. 68 7.65 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 1. 11 10. 86 19.83 29. 56 39. 15 46.62 56. 79 6 5.61 73.09 0 .00

0.00 132.76 85.10 78. 30 68.49 58.28 51. 03 41.17 30.26 21. 35 11.12 0. 75 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 4. 45 14. 41 23.35 33. 87 43. 46 50.76 60. 43 6 9.43 74.96 0 .00

18. 46 130.97 87.38 82. 49 72.92 62.48 54. 76 44.29 33.71 25. 25 14.93 3. 81 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 8. 09 18. 20 26.82 36. 94 47. 00 54.62 64. 62 7 4.15 80.18 0 .00

0.00 145.90 93.87 87. 76 77.87 66.44 59. 18 48.64 37.34 28. 55 17.11 6. 39 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.1 6 10. 26 21. 39 30.34 41. 21 51. 44 58.74 69. 63 7 8.74 83.59 0 .00

20. 07 144.95 96.71 91. 58 81.66 70.60 64. 33 53.88 41.36 32. 50 20.45 8. 83 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 2.2 7 13. 56 25. 22 34.22 46. 21 56. 37 62.75 73. 30 8 3.14 89.27 0 .00

0.00 162.60 102. 78 96. 92 86.40 74.64 68. 67 57.38 45.53 36. 10 24.10 11.75 0.27 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 5.1 3 17. 16 28. 83 38.33 49. 73 60. 74 66.93 78. 12 8 7.79 92.29 0 .00

22. 29 159.49 105. 41 102.78 92.97 79.43 73. 38 61.38 49.50 38. 45 26.58 14.94 3.51 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 8.3 3 19. 68 31. 28 42.15 53. 66 65. 19 71.35 84. 37 9 4.44 98.79 0 .00

0.00 176.47 112. 08 108.83 97.70 84.89 77. 34 65.61 53.32 41. 86 30.11 17.99 6.44 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.46 11.29 23. 14 34. 69 45.97 57. 96 69. 40 77.06 89. 35 9 9.69 101. 90 0 .00

24. 36 173.08 116. 14 114.01 102.61 90.74 80. 30 68.74 57.13 46. 12 34.27 21.45 10. 16 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 3.04 14.64 27. 20 38. 91 49.85 61. 15 72. 38 82.55 94. 08 105.58 109. 32 0 .00

0.00 191.46 126. 48 119.59 107.74 95.66 84. 26 72.96 60.66 49. 93 37.24 24.86 14. 05 0.62 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 6.70 18.01 30. 13 42. 64 53.39 65. 48 76. 63 87.81 99. 45 110.24 115. 28 0 .00

26. 75 188.04 131. 62 122.82 112.05 100. 85 88. 90 78.47 64.89 54. 41 41.36 28.06 16. 69 2.37 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 9.15 21.05 34. 12 47. 00 57.59 70. 91 81. 23 92.79 103 .64 114.46 124. 57 0 .00

0.00 209.67 139. 90 128.00 117.11 105. 06 92. 82 83.04 69.67 59. 21 46.07 31.73 20. 05 5.39 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 12. 35 24.54 38. 64 51. 70 62.37 75. 55 85. 42 97.44 109 .06 118.97 128. 51 0 .00

29. 54 207.03 142. 76 132.56 123.97 110. 30 98. 09 88.43 74.44 63. 26 49.35 35.39 23. 36 8.89 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 1. 08 15. 60 28.08 41. 82 55. 63 66.99 80. 80 90. 53 102. 49 115 .86 124.73 136. 01 0 .00

0.00 230.92 149. 59 137.40 129.59 116. 09 103.86 94.44 79.19 68. 07 53.72 38.78 25. 95 11.14 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 18. 07 31.25 45. 99 60. 28 71.67 86. 82 96. 56 108. 81 121 .95 128.95 138. 48 0 .00

31. 63 227.35 152. 08 142.46 135.87 122. 33 109.33 99.12 83.89 73. 41 58.73 42.20 29. 15 14.29 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 5. 95 21. 10 34.49 50. 76 65. 47 76.38 91. 47 101.86 114. 73 128 .14 135.44 146. 95 0 .00

0.00 250.42 161. 91 149.64 142.73 127. 89 115.84 105.15 88.78 77. 97 61.75 45.47 32. 13 17.72 0. 25 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 9. 10 23. 97 37.64 53. 67 69. 84 81.12 97. 47 108.58 120. 86 135 .57 142.07 152. 21 0 .00

35. 35 244.09 165. 79 155.12 148.45 133. 75 124.52 112.42 93.97 82. 87 65.71 48.89 34. 12 19.31 2. 65 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 10. 53 25. 86 40.78 57. 45 74. 52 86.12 104 .51 117.01 126. 67 141 .43 148.99 161. 67 0 .00

0.00 268.82 175. 55 162.73 155.67 139. 78 132.57 117.43 99.81 87. 11 70.10 52.65 37. 47 22.49 4. 76 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 13. 43 28. 92 44.25 61. 62 78. 64 91.86 109 .66 125.29 133. 31 149 .25 155.82 166. 07 0 .00

38. 22 261.40 179. 72 169.60 166.06 147. 30 139.99 123.03 105. 72 89. 90 73.03 56.39 41. 66 26.24 7. 63 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 16. 86 32. 71 47.77 64. 39 81. 39 97.54 115 .15 132.44 140. 53 159 .60 164.44 176. 80 0 .00

0.00 287.97 190. 04 177.16 174.84 156. 52 146.19 129.12 111. 09 93. 85 76.97 59.47 44. 89 28.41 10.95 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.9 9 18. 73 35. 49 50.51 68. 05 85. 18 102. 78 121 .28 139.01 150. 43 169 .24 171.44 181. 58 0 .00

40. 95 280.69 193. 53 185.72 183.87 166. 55 151.52 134.44 116. 00 98. 20 82.32 62.68 49. 08 32.60 12.84 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 2.3 7 22. 38 39. 12 53.38 72. 99 89. 37 107. 57 126 .39 144.17 160. 18 178 .54 182.29 192. 05 0 .00

0.00 310.23 204. 08 200.13 193.03 174. 85 158.15 140.56 120. 14 101.81 86.34 66.23 54. 29 37.38 15.24 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 4.2 2 26. 51 43. 61 56.56 76. 60 92. 73 111. 56 132 .37 150.97 169. 11 188 .72 197.10 196. 62 0 .00

66. 78 301.97 205. 55 214.26 210.48 175. 50 165.11 158.23 114. 91 106.32 103.68 57.33 58. 75 56.00 1. 24 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 42. 64 47. 26 48.60 92. 00 96. 93 107. 45 148 .20 157.34 170. 17 204 .33 213.72 210. 67 0 .00

0.00 345.62 220. 31 228.88 254.97 145. 32 165.10 207.52 68.40 102.56 156.23 0. 26 54. 69 116.96 0. 00 0.00 70.42 0. 00 0.00 5.43 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 49.62 0.00 94. 72 41. 70 0.7 0 137 .63 92. 68 66.55 190 .96 157.03 145. 88 242 .88 227.81 226. 39 0 .00

0.00 345.62 220. 31 228.88 254.97 145. 32 165.10 207.52 68.40 102.56 156.23 0. 26 54. 69 116.96 0. 00 0.00 70.42 0. 00 0.00 5.43 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 49.62 0.00 0.0 0 94. 72 41. 70 0.7 0 137 .63 92. 68 66.55 190 .96 157.03 145. 88 242 .88 227.81 226. 39 0 .00

0.00 421.51 0. 00 855.14 0.00 0. 00 590.64 0.00 0. 00 339.67 0.00 0. 00 181.73 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 135.69 0.0 0 0. 00 309.98 0.0 0 0 .00 564.40 0.0 0 0 .00 842.19 0. 00 0 .00

0.00 421.51 0. 00 855.14 0.00 0. 00 590.64 0.00 0. 00 339.67 0.00 0. 00 181.73 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 135.69 0.0 0 0. 00 309.98 0.0 0 0 .00 564.40 0.0 0 0 .00 842.19 0. 00 0 .00

0.00 421.51 0. 00 859.34 0.00 0. 00 594.99 0.00 0. 00 344.02 0.00 0. 00 186.54 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 140.50 0.0 0 0. 00 314.34 0.0 0 0 .00 568.75 0.0 0 0 .00 846.40 0. 00 0 .00

0.00 421.51 0. 00 859.34 0.00 0. 00 594.99 0.00 0. 00 344.02 0.00 0. 00 186.54 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 140.50 0.0 0 0. 00 314.34 0.0 0 0 .00 568.75 0.0 0 0 .00 846.40 0. 00 0 .00

0.00 495.70 0. 00 940.67 0.00 0. 00 642.90 0.00 0. 00 354.11 0.00 0. 00 193.58 0.00 0. 00 29. 03 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 160.70 0.0 0 0. 00 323.47 0.0 0 0 .00 614.10 0.0 0 0 .00 913.50 0. 00 0 .00

0.00 511.35 0. 00 1032. 83 0.00 0. 00 664.73 0.00 0. 00 305.07 0.00 0. 00 171.01 0.00 0. 00 64. 36 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 14. 05 0.0 0 0. 00 144.31 0.0 0 0. 00 279.76 0.0 0 0 .00 629.93 0.0 0 0 .00 996.28 0. 00 0 .00

0.00 546.66 0. 00 1212. 59 0.00 0. 00 690.86 0.00 0. 00 225.82 0.00 0. 00 177.22 0.00 0. 00 165.49 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 105.82 0.0 0 0. 00 137.48 0.0 0 0. 00 204.15 0.0 0 0 .00 649.91 0.0 0 0 .00 115 3.81 0. 00 0 .00

0.00 549.26 0. 00 930.16 0.00 0. 00 676.69 0.00 0. 00 534.76 0.00 0. 00 155.14 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 110.15 0.0 0 0. 00 478.14 0.0 0 0 .00 630.73 0.0 0 0 .00 884.84 0. 00 0 .00

0.00 791.21 0. 00 914.64 0.00 0. 00 649.06 0.00 0. 00 503.36 0.00 0. 00 157.67 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 99. 95 0.0 0 0. 00 442.55 0.0 0 0 .00 598.54 0.0 0 0 .00 864.67 0. 00 0 .00

0.00 783.56 0. 00 1027. 81 0.00 0. 00 636.62 0.00 0. 00 459.69 0.00 0. 00 144.74 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 81. 40 0.0 0 0. 00 388.15 0.0 0 0 .00 575.97 0.0 0 0 .00 958.56 0. 00 0 .00

0.00 767.51 0. 00 995.79 0.00 0. 00 692.39 0.00 0. 00 424.48 0.00 0. 00 104.20 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 32. 33 0.0 0 0. 00 344.59 0.0 0 0 .00 611.17 0.0 0 0 .00 919.31 0. 00 0 .00

0.00 0.00 0. 00 971.16 0.00 0. 00 0.00 0.00 0. 00 423.25 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 343.88 0.0 0 0 .00 0.00 0.0 0 0 .00 893.52 0. 00 0 .00

240-249 250-259200-209 210-219 220-229 230-2390.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

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0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.10 1.59 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.10 6.80 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

1.01 9.39 1. 98 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 13.65 4. 67 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

2.45 18.11 6. 85 2.52 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 28.43 14.73 9.12 2.63 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

5.89 50.49 19.58 13. 16 7.28 0. 30 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 57.03 35.80 26. 99 16.11 3. 04 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 55.13 34.25 25. 25 14.18 0. 96 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

12. 19 53.61 50.05 38. 74 22.10 4. 03 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 81.10 50.55 41. 41 26.62 11.54 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

9.91 80.46 53.12 45. 40 31.81 17.16 0.27 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 88.18 57.63 50. 23 37.60 22.82 5.87 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

11. 06 87.02 59.48 53. 84 42.49 29.33 12. 51 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 97.01 64.82 58. 61 47.62 34.73 17. 74 0.14 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

12. 00 96.15 70.13 63. 52 53.55 40.64 23. 88 6.39 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

0.00 107.45 77.13 67. 85 58.21 46.95 30. 82 13.08 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 1 .03

13. 50 107.93 80.90 73. 07 64.23 52.48 36. 58 17.99 0. 30 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 6 .01

0.00 120.97 87.29 79. 98 71.53 58.42 42. 74 24.00 4. 70 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 9 .27

15. 16 121.25 89.79 85. 51 77.76 65.88 49. 17 30.86 10.63 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 37 15. 34

0.00 136.35 96.28 91. 87 83.82 72.53 54. 11 36.25 17.21 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 3. 98 18. 29

17. 24 137.06 100. 91 98. 58 90.62 79.47 60. 52 42.69 22.64 1.14 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 8. 73 25. 13

0.00 153.92 108. 50 104.82 95.89 86.36 68. 13 50.03 28.70 6.99 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.39 12.19 28. 90

19. 04 154.38 112. 93 111.05 102.80 92.38 74. 72 55.79 35.44 13. 49 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 4.77 16.87 37. 17

0.00 171.35 121. 60 118.54 111.08 99.05 81. 95 62.78 41.35 18. 60 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 9.70 20.84 39. 37

21. 44 170.51 125. 17 124.22 118.27 107. 30 90. 03 70.78 47.90 24. 89 0.11 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .62 1 3.85 25.09 47. 53

0.00 189.78 133. 46 131.65 125.65 114. 55 96. 62 76.88 55.11 31. 92 6.82 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 4 .74 1 8.74 28.97 50. 05

23. 84 188.48 139. 25 139.49 134.62 122. 35 104.17 84.23 61.40 37. 27 11.30 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 10. 79 2 4.60 34.94 59. 98

0.00 208.79 149. 44 147.09 141.57 130. 97 112.10 92.84 68.25 43. 60 16.96 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 15. 27 2 9.11 39.06 62. 77

26. 09 207.13 155. 18 154.98 149.50 139. 55 118.93 99.70 75.90 50. 68 23.42 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 3.3 5 20. 83 3 4.87 45.45 74. 18

0.00 228.85 166. 71 164.88 157.80 148. 31 127.56 107.59 82.64 56. 18 27.77 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 9.4 1 27. 42 4 1.31 50.81 76. 46

28. 41 226.95 172. 02 172.86 165.11 158. 22 138.50 116.28 90.02 62. 92 33.81 3. 05 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 16.26 32. 37 4 6.71 56.92 89. 50

0.00 251.62 183. 11 182.18 173.84 166. 65 147.98 122.85 98.29 70. 52 40.74 8. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 1.21 22.49 38. 91 5 2.54 61.27 92. 02

31. 06 250.17 189. 61 191.26 185.34 176. 56 157.58 131.36 105. 50 76. 26 45.21 13.20 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 7.94 29.51 46. 44 5 9.44 68.56 106 .28

0.00 277.40 200. 75 200.13 194.79 188. 40 166.79 141.96 112. 97 82. 91 50.83 16.71 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 15. 58 37.64 52. 74 6 5.02 72.81 107 .69

35. 01 275.14 206. 74 209.94 205.61 200. 57 174.84 150.76 121. 19 90. 23 57.25 20.97 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 21. 85 45.13 60. 41 7 2.41 80.47 121 .91

0.00 303.06 221. 62 222.54 218.20 211. 03 185.34 160.19 128. 55 95. 71 61.18 25.61 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 3 .25 29. 89 53.61 69. 86 8 0.60 86.42 120 .39

37. 53 298.93 229. 58 233.87 230.60 221. 66 199.07 170.41 136. 39 102.26 66.80 28.75 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 11. 62 39. 37 62.39 77. 88 8 8.40 94.51 134 .54

0.00 329.51 244. 94 248.03 244.07 231. 15 211.69 179.09 144. 04 109.31 74.79 30.86 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 19. 11 48. 21 70.52 88. 65 9 7.37 99.15 131 .21

41. 05 327.08 255. 36 263.82 260.07 243. 51 224.66 190.23 149. 08 114.39 81.50 31.34 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 29. 34 58. 61 79.91 101 .37 109.17 109. 14 150 .24

0.00 368.75 275. 21 281.26 283.97 246. 69 236.89 219.92 136. 98 120.37 112.01 6. 97 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 61. 35 69. 47 77.54 127 .93 122.33 112. 81 172 .77

0.00 932.40 35.80 28. 71 15.34 153. 92 110.42 59.98 141. 57 9.41 137.69 0. 00 0.00 1.21 0. 00 0.00 22.49 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 38. 91 0.00 0.0 0 185 .34 59. 44 0.0 0 303 .06 298.93 41.05 69. 47

0.00 932.40 35.80 28. 71 15.34 153. 92 110.42 59.98 141. 57 9.41 137.69 0. 00 0.00 1.21 0. 00 0.00 22.49 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 38. 91 0.00 0.0 0 185 .34 59. 44 0.0 0 303 .06 298.93 41.05 69. 47

0.00 122.33 0. 00 58. 61 0.00 0. 00 124.22 0.00 0. 00 541.79 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 12. 25 0.0 0 0 .00 221.66 0. 00 127 .93

0.00 122.33 0. 00 58. 61 0.00 0. 00 124.22 0.00 0. 00 541.79 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 12. 25 0.0 0 0 .00 221.66 0. 00 127 .93

0.00 122.33 0. 00 64. 82 0.00 0. 00 125.17 0.00 0. 00 354.51 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 184.63 0.0 0 0 .00 230.60 0. 00 127 .93

0.00 122.33 0. 00 64. 82 0.00 0. 00 125.17 0.00 0. 00 354.51 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 184.63 0.0 0 0 .00 230.60 0. 00 127 .93

0.00 498.72 0. 00 1198. 11 0.00 0. 00 865.61 0.00 0. 00 380.40 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 342.69 0.0 0 0 .00 725.13 0. 00 333 .20

0.00 543.82 0. 00 1315. 96 0.00 0. 00 926.79 0.00 0. 00 316.65 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 401.84 0.0 0 0 .00 842.57 0. 00 354 .51

0.00 572.38 0. 00 1496. 22 0.00 0. 00 964.13 0.00 0. 00 248.51 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 442.83 0.0 0 0 .00 102 0.31 0. 00 327 .77

0.00 573.57 0. 00 1219. 10 0.00 0. 00 932.40 0.00 0. 00 594.11 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 122.33 0.0 0 0 .00 418.49 0.0 0 0 .00 753.25 0. 00 327

0.00 834.17 0. 00 1200. 36 0.00 0. 00 883.72 0.00 0. 00 549.59 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 77. 34 0.0 0 0 .00 378.22 0.0 0 0 .00 720.57 0. 00 649

0.00 828.04 0. 00 1331. 37 0.00 0. 00 836.26 0.00 0. 00 491.37 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 17. 62 0.0 0 0 .00 347.03 0.0 0 0 .00 830.79 0. 00 631

0.00 815.87 0. 00 1296. 50 0.00 0. 00 857.01 0.00 0. 00 433.66 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 351.09 0.0 0 0 .00 751.75 0. 00 591

0.00 0.00 0. 00 1255. 87 0.00 0. 00 0.00 0.00 0. 00 433.34 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 721.08 0. 00 0

340-349 350-359300-309 310-319 320-329 330-3390.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 0.00 0.0 0 0 .00 0.00 0. 00 0 .00

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0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .00 1.44 6.3 4 11. 56 1 6.84 21.43 37. 71

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0 .44 5.23 10.12 14. 25 1 9.47 24.32 39. 55

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 3 .09 8.39 13.84 17. 78 2 3.07 28.39 46. 56

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.3 1 6 .23 11. 86 17.54 21. 95 2 7.12 32.18 46. 93

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 9 .55 15. 27 21.03 25. 07 3 0.93 36.97 54. 71

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 5.2 2 11. 52 18. 25 25.20 29. 41 3 5.04 39.96 58. 76

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 2.38 8.6 7 15. 32 22. 23 29.56 35. 12 4 0.91 47.16 73. 95

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 14 5.74 12.47 18. 89 25. 06 32.30 38. 83 4 4.53 50.80 90. 93

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 97 8.93 16.78 25. 10 31. 23 39.32 47. 44 5 5.88 62.72 99. 79

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 31 7.62 15.47 23. 79 30. 03 38.11 46. 23 5 4.67 61.56 98. 19

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 1. 95 11. 03 20.00 29. 67 37. 79 46.81 53. 87 6 3.82 72.27 92. 09

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 4. 13 13. 48 22.87 32. 80 42. 11 51.90 56. 77 6 6.42 76.15 121 .62

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 7. 40 17. 01 26.63 35. 97 45. 84 56.20 61. 45 7 0.96 80.10 119 .72

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.8 3 10. 13 19. 92 29.70 39. 55 49. 51 59.64 66. 85 7 6.60 87.11 130 .22

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 4.2 5 13. 86 23. 48 33.12 43. 43 53. 33 63.00 71. 34 8 0.60 90.01 126 .38

0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 7.9 3 17. 99 27. 59 36.80 46. 55 56. 47 66.02 75. 41 8 5.10 95.39 140 .74

0.00 0.74 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 2.39 11.40 21. 03 31. 26 40.19 50. 56 60. 45 69.85 79. 82 8 9.09 97.53 139 .35

0.22 3.71 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 5.21 14.67 25. 04 35. 43 43.99 55. 18 65. 08 73.56 83. 22 9 3.08 103. 01 155 .07

0.00 8.12 0. 28 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 8.78 18.30 29. 42 39. 74 48.04 58. 81 69. 41 77.16 87. 68 9 7.17 105. 42 152 .89

0.82 10.93 2. 67 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 75 12. 37 21.89 32. 55 43. 35 52.05 63. 18 73. 94 81.07 92. 95 103.01 111. 23 169 .53

0.00 15.93 5. 21 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 3. 16 15. 07 25.10 36. 54 47. 57 56.06 68. 19 78. 93 85.90 97. 35 107.52 112. 57 167 .40

2.05 19.34 8. 05 1.87 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 6. 76 18. 59 28.50 41. 08 52. 21 59.95 71. 83 83. 08 90.43 102 .03 113.01 119. 02 185 .88

0.00 26.02 11.93 5.36 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 10. 48 21. 97 31.75 43. 91 56. 16 63.97 76. 67 88. 23 95.09 107 .79 118.08 122. 34 182 .87

3.36 29.03 14.54 8.11 0.88 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.5 5 12. 53 24. 27 35.03 47. 54 60. 42 68.26 82. 57 94. 01 99.48 112 .00 123.24 129. 35 203 .50

0.00 36.48 18.03 11. 42 3.97 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 3.4 4 15. 89 27. 51 38.50 51. 50 64. 19 73.26 86. 85 99. 25 104. 26 117 .47 128.41 131. 84 200 .94

4.73 38.88 21.48 15. 45 7.73 0. 21 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 6.7 3 19. 91 31. 33 42.02 54. 36 66. 86 78.30 91. 17 104.08 108. 99 124 .64 136.25 139. 98 220 .21

0.00 46.33 24.99 18. 94 10.85 2. 94 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 9.8 2 22. 73 34. 74 45.29 58. 32 70. 81 82.82 95. 87 108.47 115. 74 130 .53 142.31 142. 87 214 .24

6.14 48.25 28.21 22. 54 14.42 5. 95 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 12.75 26. 54 38. 93 49.01 63. 07 75. 77 87.06 99. 40 111.59 122. 48 135 .67 148.98 151. 85 236 .12

0.00 57.10 33.58 26. 68 18.39 9. 40 0.52 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.76 16.11 30. 34 43. 60 52.84 66. 56 80. 22 90.94 104 .28 116.31 128. 56 141 .52 153.71 158. 30 230 .17

7.76 59.53 37.35 29. 96 21.81 13.53 4.41 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 4.05 19.61 32. 16 47. 04 56.47 71. 03 85. 17 95.56 110 .53 121.23 133. 94 146 .04 158.27 169. 96 254 .20

0.00 70.61 42.57 34. 26 25.90 16.86 7.48 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 5.66 22.41 35. 45 50. 76 60.43 76. 23 90. 48 100. 94 115 .92 125.78 139. 10 152 .09 162.93 173. 42 250 .41

9.67 72.86 46.79 39. 01 31.06 20.94 11. 22 1.23 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 8.38 25.43 39. 71 54. 15 64.59 80. 03 95. 06 106. 28 121 .69 131.28 144. 47 159 .65 169.08 182. 09 277 .99

0.00 85.19 51.90 43. 35 35.46 25.67 15. 51 5.18 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 11. 45 28.09 42. 76 56. 75 68.46 84. 83 100.36 111. 41 128 .38 137.92 151. 43 166 .50 173.27 183. 65 273 .63

11. 48 88.70 55.93 48. 09 40.41 29.90 19. 16 8.36 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 13. 63 30.47 46. 39 60. 10 72.10 90. 46 106.35 116. 49 133 .53 143.77 157. 92 173 .04 180.28 193. 56 301 .26

0.00 103.41 63.42 54. 19 46.02 34.34 23. 42 12.18 0. 46 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 16. 64 33.38 50. 41 63. 19 75.85 93. 95 111.45 121. 70 140 .08 151.28 164. 50 181 .06 187.19 198. 46 293 .61

14. 05 106.64 68.36 59. 43 51.15 39.63 28. 75 16.51 3. 09 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 15 19. 58 36.21 52. 49 65. 32 79.90 98. 04 116.54 127. 07 147 .92 160.90 170. 42 187 .19 194.67 209. 38 322 .47

0.00 123.58 76.58 66. 16 57.12 44.17 33. 28 19.71 6. 49 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 67 21. 26 38.92 55. 80 68. 91 83.96 102 .52 120.75 133. 64 153 .69 170.51 177. 46 195 .42 201.61 212. 93 313 .97

16. 44 127.39 83.26 73. 20 64.74 49.48 38. 03 23.48 9. 09 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 2. 84 24. 05 42.23 59. 60 73. 52 87.83 105 .60 123.63 140. 51 159 .58 178.23 184. 97 206 .55 210.56 225. 07 344 .43

0.00 148.04 92.62 80. 33 71.53 55.84 42. 72 27.60 12.10 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 5. 60 27. 39 46.14 61. 66 77. 11 90.94 109 .74 127.78 146. 45 166 .20 185.17 195. 98 216 .86 217.31 228. 88 335 .81

18. 70 155.66 100. 19 88. 31 78.46 61.88 46. 43 30.76 15.37 0.24 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 7. 17 28. 99 48.56 65. 62 81. 48 94.20 115 .45 132.26 151. 67 171 .81 190.75 207. 38 225 .67 228.08 240. 59 370 .43

0.00 184.61 111. 60 99. 37 85.48 67.36 50. 66 34.36 17.67 2.13 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 10.68 31. 83 51.00 70. 12 87. 12 97.82 119 .65 135.85 156. 00 178 .31 198.61 218. 83 234 .48 242.16 244. 66 363 .09

34. 30 204.18 117. 87 108.13 93.51 70.94 54. 95 42.17 17.14 4.52 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 34.01 35. 14 37.62 87. 55 92. 03 89.68 136 .09 140.42 151. 72 195 .29 205.84 220. 47 251 .37 260.14 259. 53 401 .78

0.00 204.95 148. 54 119.25 106.04 62.44 50. 32 68.15 0. 77 1.68 26.16 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 41.94 0.00 0.0 0 106. 09 26. 83 0.0 0 144 .05 87. 50 35.45 185 .35 136.54 108. 42 241 .34 204.91 191. 76 294 .91 277.73 274. 49 419 .34

0.00 204.95 148. 54 119.25 106.04 62.44 50. 32 68.15 0. 77 1.68 26.16 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 41.94 0.00 0.0 0 106. 09 26. 83 0.0 0 144 .05 87. 50 35.45 185 .35 136.54 108. 42 241 .34 204.91 191. 76 294 .91 277.73 274. 49 419 .34

0.00 216.74 0. 00 448.74 0.00 0. 00 211.42 0.00 0. 00 12. 22 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 105.77 0.0 0 0. 00 277.84 0.0 0 0. 00 449.00 0.0 0 0 .00 716.16 0.0 0 0 .00 100 3.81 0. 00 477 .71

0.00 216.74 0. 00 448.74 0.00 0. 00 211.42 0.00 0. 00 12. 22 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 105.77 0.0 0 0. 00 277.84 0.0 0 0. 00 449.00 0.0 0 0 .00 716.16 0.0 0 0 .00 100 3.81 0. 00 477 .71

0.00 216.74 0. 00 444.53 0.00 0. 00 207.06 0.00 0. 00 7.87 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 99. 92 0.0 0 0. 00 273.03 0.0 0 0. 00 444.65 0.0 0 0 .00 711.81 0.0 0 0 .00 999.60 0. 00 477 .71

0.00 216.74 0. 00 444.53 0.00 0. 00 207.06 0.00 0. 00 7.87 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 99. 92 0.0 0 0. 00 273.03 0.0 0 0. 00 444.65 0.0 0 0 .00 711.81 0.0 0 0 .00 999.60 0. 00 477 .71

0.00 264.32 0. 00 470.46 0.00 0. 00 234.03 0.00 0. 00 16. 01 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 145.79 0.0 0 0. 00 300.12 0.0 0 0. 00 459.69 0.0 0 0 .00 763.29 0.0 0 0 .00 107 4.53 0. 00 561 .56

0.00 311.98 0. 00 531.76 0.00 0. 00 251.04 0.00 0. 00 1.85 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 207.97 0.0 0 0. 00 311.04 0.0 0 0. 00 441.94 0.0 0 0 .00 804.49 0.0 0 0 .00 118 4.84 0. 00 610 .43

0.00 373.53 0. 00 651.14 0.00 0. 00 260.51 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 309.51 0.0 0 0. 00 309.59 0.0 0 0. 00 371.41 0.0 0 0 .00 825.71 0.0 0 0 .00 136 1.31 0. 00 615 .62

0.00 356.22 0. 00 486.91 0.00 0. 00 250.55 0.00 0. 00 161.10 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 293.57 0.0 0 0. 00 652.66 0.0 0 0 .00 817.30 0.0 0 0 .00 106 3.22 0. 00 620 .40

0.00 499.00 0. 00 473.58 0.00 0. 00 230.63 0.00 0. 00 137.28 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 291.22 0.0 0 0. 00 629.25 0.0 0 0 .00 797.08 0.0 0 0 .00 105 4.15 0. 00 853 .39

0.00 482.69 0. 00 522.85 0.00 0. 00 205.82 0.00 0. 00 78. 56 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 273.48 0.0 0 0. 00 577.53 0.0 0 0 .00 777.52 0.0 0 0 .00 115 8.69 0. 00 840 .76

0.00 467.10 0. 00 491.21 0.00 0. 00 237.77 0.00 0. 00 44. 43 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 234.06 0.0 0 0. 00 543.60 0.0 0 0 .00 823.31 0.0 0 0 .00 112 7.73 0. 00 825 .11

0.00 0.00 0. 00 470.80 0.00 0. 00 0.00 0.00 0. 00 40. 26 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.00 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 0.00 0.0 0 0. 00 543.51 0.0 0 0 .00 0.00 0.0 0 0 .00 110 1.74 0. 00 0 .00

440-449 450-459400-419 410-419 420-429 430-439

.92

.85

.12

.85

.00

SouthNorth East West

Page 49: Baseline Structural Performance and Aircraft Impact Damage

Results of Baseline Analysis for Typical Results of Baseline Analysis for Typical TrussTruss--Framed Floor (Floor 96)Framed Floor (Floor 96)

DCRs for Structural Components under Original WTC Design Loads

Mean % members MaxDCR with DCR<1 DCR

One-Way Long Span TrussesDiagonals 0.44 96 1.14Bottom chord members 0.74 100 0.99

One-Way Short Span TrussesDiagonals 0.33 100 0.92Bottom chord members 0.37 100 0.55

Two-Way TrussesDiagonals 0.30 99 1.06Bottom chord members 0.48 100 0.94

Core Beams 0.33 99 1.07

Page 50: Baseline Structural Performance and Aircraft Impact Damage

Key Findings: Wind LoadsKey Findings: Wind LoadsThe original design wind loads on the towers exceeded those established in the prescriptive provisions of the New York City Building Code (NYCBC) prior to 1968, when the WTC towers were designed, and up to and including 2001. The original design load estimates were also higher than those required by other selected building codes of the time (Chicago and New York State), including the relevant national model building code, Building Officials Conference America (BOCA). The prescriptive approach in these codes is oversimplified, and as a result, these codes are not necessarily appropriate for super-tall building design.

In the majority of the cases, each of the two orthogonal shear components and of the two orthogonal overturning moment components at the base of the towers used in the original wind design were smaller than the CPP, RWDI, and refined NIST estimates. However, the most unfavorable combined peaks (resultant) from the original design were larger, or smaller, by at most 15 percent than estimates based on the CPP, RWDI, and NIST estimates. This is due to the conservative approach used to combine the loads in the original design.

The estimated wind-induced loads on the towers varied by as much as 40 percent between the wind tunnel/climatological studies conducted in 2002 by CPP and RWDI. The primary reason for these differences was the different approaches used in those studies to (1) estimate extreme wind speeds; (2) estimate wind profiles; (3) integrate aerodynamic, dynamic, and extreme wind climatological information; and (4) combine wind effects in two orthogonal directions and in torsion. Such disparity is indicative of the limitations and inconsistencies associated with the current state of practice in wind engineering for tall buildings.

Page 51: Baseline Structural Performance and Aircraft Impact Damage

Key Findings: Baseline PerformanceKey Findings: Baseline PerformanceUnder the original WTC design loads, the cumulative drifts at the top of the WTC towers ranged from H/263 to H/335. For the lower-estimate SOP case, those drifts ranged from H/253 to H/306.

Under design loading conditions, the maximum inter-story drift was as high as h/230 and h/200 for WTC 1 and WTC 2, respectively, where h is the story height. Maximum inter-story drifts under the SOP case were about h/184 and h/200 for WTC 1 and WTC 2, respectively.

For the refined NIST estimate case, the cumulative and inter-story drifts were about 25 percent larger than those from the SOP case.

Current building codes do not specify a drift limit for wind design. Structural engineers often use in their practice the criterion that total drift ratios should not exceed H/400 to H/500 for serviceability considerations and to enhance overall safety and stability (including P-∆ effects). For inter-story drifts, structural engineers often use in their practice an inter-story drift limit in the range of h/300 to h/400. Similar to total drift, inter-story drifts of the towers were larger than what is generally used in current practice.

Page 52: Baseline Structural Performance and Aircraft Impact Damage

Key Findings: Baseline PerformanceKey Findings: Baseline PerformanceThe DCRs based on the allowable stress design procedure, estimated from the original WTC design load case were in general close to those obtained for the lower-estimate SOP case. For both cases, a fraction of the structural components had DCRs larger than 1.0. These were mainly observed in both towers at:

• The exterior walls: (1) at the columns around the corners, (2) where the hat truss connected to the exterior walls, and (3) below floor 9.

• The core columns on the 600 line between floors 80 and 106 and at core perimeter columns 901 and 908 for much of their height.

The DCRs obtained for the refined NIST estimate case were higher than those for the original WTC design and the lower-estimate SOP load cases, owing to:

• The NIST estimated wind loads were larger than those used in the state-of-the-practice case by about 25 percent

• The original WTC design and the SOP cases used NYCBC load combinations, which result in lower DCRs than the ASCE 7-02 load combinations used for the refined NIST case.

The safety of the WTC towers on September 11, 2001 was most likely not affected by the fraction of members for which the demand exceeded allowable capacity due to: (1) the inherent factor of safety in the allowable stress design method, (2) the load redistribution capability of ductile steel structures, and (3) on the day of the attack, the towers were subjected to in-service live loads (a fraction of the design live loads) and minimal wind loads.

Page 53: Baseline Structural Performance and Aircraft Impact Damage

Aircraft Impact AnalysisAircraft Impact AnalysisBuildings are not specifically designed to withstand the impact of fuel-laden commercial aircraft, and building codes in the United States do not require building designs to consider aircraft impact.

Documents obtained from The Port Authority of New York and New Jersey indicated that the safety of the WTC towers and their occupants in an aircraft collision was a consideration in the original design. Such documents include:

• Port Authority (February 1964), three-page white paper, “Salient points with regard to the structural design of The World Trade Center towers,” dated 2-3-64.

• Port Authority (March 1964), three-page document, “period of vibration due to plane crash at 80th floor.”

• Alternative Insurance Works (2001), World Trade Center Property Risk Report, Prepared for Silverstein Properties, Inc.

• The New Yorker (11/19/2001), “The Tower Builder” by John Seabrook, Interview with Leslie Robertson.

• FEMA 403 (2002), World Trade Center Building Performance Study: Data Collection, Preliminary Observations, and Recommendations.

• Glanz and Lipton (2003), City in the Sky – The Rise and the Fall of The – World Trade Center, Times Books, 2003.

Page 54: Baseline Structural Performance and Aircraft Impact Damage

Aircraft Impact AnalysisAircraft Impact AnalysisThe documents indicate that a Boeing 707, the largest commercial aircraft at the time, flying at 600 mph was considered and that the analysis indicated that such collision would result in only local damage which could not cause collapse or substantial damage to the building and would not endanger the lives and safety of occupants not in the immediate area of impact.

No documentary evidence of the aircraft impact analysis was available to review the criteria and methods used in the analysis of the aircraft impact into the WTC towers, or to provide details on the ability of the WTC towers to withstand such impacts.

Page 55: Baseline Structural Performance and Aircraft Impact Damage

Aircraft Impact Analysis ObjectivesAircraft Impact Analysis Objectives

Provide estimates of probable damage to structural systems, including exterior walls, floor systems, and interior core columns

Provide estimates of the aircraft fuel dispersion during the impact

Provide estimates of debris damage to the building nonstructural contents, including partitions and workstations. The results were to be used to estimate the damage to fireproofing.

Establish the initial conditions for the fire dynamics modeling and thermal-structural response and collapse initiation analyses.

Page 56: Baseline Structural Performance and Aircraft Impact Damage

Technical ApproachTechnical Approach

Reference Structural Models of the Towers

Material Constitutive and Failure Modeling

WTC Towers Model Development

Aircraft Data Collection and Model Development

Component Impact Analyses

Subassembly Analysis

Aircraft Impact Initial Conditions

Sensitivity Analysis

Global Impact Analyses