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Hong Kong University of Science and Technol Hong Kong University of Science and Technol Department of Mathematics Department of Mathematics Presented by HUI Kin Yip Ronald HUI Kin Yip Ronald
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The Hong Kong University of Science and Technology

Jan 13, 2016

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The Hong Kong University of Science and Technology. Department of Mathematics. Presented by. HUI Kin Yip Ronald. Low Level Wind Field Analysis Around an International Airport. Contents. Introduction and Background Methodology LLWAS model Ideal Cases Gust Front model Microburst model - PowerPoint PPT Presentation
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Page 1: The Hong Kong University of Science and Technology

The Hong Kong University of Science and TechnologyThe Hong Kong University of Science and Technology

Department of MathematicsDepartment of Mathematics

Presented by

HUI Kin Yip RonaldHUI Kin Yip Ronald

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Low Level Wind Field AnalysisLow Level Wind Field Analysis AroundAround

an International Airportan International Airport

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ContentsContents

Introduction and BackgroundIntroduction and BackgroundMethodologyMethodologyLLWAS modelLLWAS modelIdeal CasesIdeal Cases

Gust Front modelGust Front model Microburst modelMicroburst model

Real CasesReal CasesConclusionsConclusions

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What is Windshear?What is Windshear?Any change of wind speed and/or directionAny change of wind speed and/or directionCan appear Can appear suddenlysuddenly in thunderstorms in thunderstormsAssociated with Associated with gust frontsgust fronts and and microburstsmicrobursts

Why is windshear so dangerous?Why is windshear so dangerous?Dangerous when an aircraft near the groundDangerous when an aircraft near the groundUnbalanced forces appeared suddenlyUnbalanced forces appeared suddenlyDifficult to predictDifficult to predictHard for a pilot to make correctionsHard for a pilot to make corrections

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CRASH!!!

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Civil aviation accident cause

U.S. Domestic Jet Crashes 1975-94

CircumstanceNo. of Major

crashNo. of Deaths

Thunderstorm wind shear 4 419

Collision ( ground and air ) 3 159

Ice buildup 3 122

DC-10 hydraulic failure 2 371

Takeoff without flaps 2 161

Unknown cause 2 147

Engine loss in flight 1 69

Sabotage 1 39

Engine loss on takeoff 1 31

Total 19 1518

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ObjectivesObjectives

Study the model of a windshear Study the model of a windshear alerting system and test in real time alerting system and test in real time situation by studying the wind field situation by studying the wind field modelmodel

Design a windshear warning systemDesign a windshear warning systemDetect the occurrence of strong Detect the occurrence of strong

windshearwindshearReal case test of system on the Bai-Real case test of system on the Bai-

yun International Airport in yun International Airport in Guangzhou, ChinaGuangzhou, China

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MethodologyMethodology

Use Use Automatic Automatic Weather Weather Station Station (AWS)(AWS)

It is low-cost, easy to maintain and It is low-cost, easy to maintain and easy to install at any placeseasy to install at any places

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Introduction and History of LLWASIntroduction and History of LLWAS

LLWAS = Low Level Windshear LLWAS = Low Level Windshear Alerting SystemAlerting System

Developed in 1970s by the US Developed in 1970s by the US GovernmentGovernment

Developed under the Joint Airport Developed under the Joint Airport Weather Studies (JAWS)Weather Studies (JAWS)

Started at Denver, Colorado in 1982Started at Denver, Colorado in 1982Most commonly used method for Most commonly used method for

detecting windshear in US nowadaysdetecting windshear in US nowadaysIt is not well-tested in Asia-Pacific regionIt is not well-tested in Asia-Pacific region

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Methodology on Ideal CaseMethodology on Ideal CaseOnly two phenomena will be focusedOnly two phenomena will be focused

Gust FrontGust Front MicroburstMicroburst

minmax-GWD vv

Calculation of Global Calculation of Global Wind Difference (GWD)Wind Difference (GWD)

RUNWAY

START

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““A leading edge of a mesoscale pressure A leading edge of a mesoscale pressure dome followed by a surge of gusty dome followed by a surge of gusty winds on or near the ground” winds on or near the ground” (Wakimoto, 1982)(Wakimoto, 1982)

Typical length = 12 km (along front) Typical length = 12 km (along front) and 0.5 km (across front)and 0.5 km (across front)

Propagation speed = 5 to 20 m/s (Uyeda Propagation speed = 5 to 20 m/s (Uyeda and Zrnic, 1985)and Zrnic, 1985)

Gust FrontGust Front

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Assumptions:Assumptions: Wind speed at Wind speed at

head = 0 m/shead = 0 m/s Wind speed in the Wind speed in the

front = 10 m/sfront = 10 m/s Wind speed is Wind speed is

increasing linearly increasing linearly for 400 mfor 400 m

The front is The front is propagating in a propagating in a constant directionconstant direction

Gust Front ModelGust Front Model

Background wind Background wind speed is addedspeed is added

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Skew angleSkew angle of a g of a gust front is the angust front is the angle between the runle between the runway and the path way and the path of the gustof the gust

Different skew anDifferent skew angles of the gust frogles of the gust fronts are appliednts are applied

GWD values of GWD values of different gust different gust locations are locations are calculated in both calculated in both casescases

ComparisonsComparisons

Gust head

Gust head

Gust head

Direction of gust

Runway

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Gust Front with 0° skew angleGust Front with 0° skew angle

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Gust Front with 30° skew angleGust Front with 30° skew angle

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Gust Front with 90° skew angleGust Front with 90° skew angle

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Facts:Facts: Errors apeared near the ends of the runway Errors apeared near the ends of the runway

when the skew angle is smallwhen the skew angle is small Errors near the centre of the runway increaErrors near the centre of the runway increa

ses with the skew angleses with the skew angle Maximum error Maximum error 3 m/s 3 m/s

Conclusion:Conclusion: Reasonable estimate for the gust passing Reasonable estimate for the gust passing

through the runway nearly from one end to through the runway nearly from one end to anotheranother

ResultsResults

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““An outward-moving airflow induced An outward-moving airflow induced by the evaporatively cooled downdraft by the evaporatively cooled downdraft from a thunderstorm or heavy rain.”from a thunderstorm or heavy rain.”

MicroburstMicroburst

Typical Typical duration duration = 10 min= 10 min

Typical Typical radius = radius = 2 to 3 km2 to 3 km

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A simplified mathematical microburst model A simplified mathematical microburst model from Wilson and Flueck (1986) is usedfrom Wilson and Flueck (1986) is used

Assumptions:Assumptions: it satisfies the mass continuity equationit satisfies the mass continuity equation it exhibits realistic radial outflow at ground levelit exhibits realistic radial outflow at ground level it is symmetric about its centreit is symmetric about its centre it is radially symmetric about the originit is radially symmetric about the origin

Microburst ModelMicroburst Model

Background wind speed is addedBackground wind speed is added

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Microburst ModelMicroburst Model

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8 different locatio8 different locationsns Locations of the Locations of the

microbursts are microbursts are lying on a line lying on a line perpendicular to perpendicular to the runwaythe runway

10 different size o10 different size of the microburstsf the microbursts Radius of Radius of

microburst = 1.8 microburst = 1.8 to 3.8 kmto 3.8 km

ComparisonsComparisons

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Facts:Facts: Both 16-AWS and 18-AWS networks give reasonaBoth 16-AWS and 18-AWS networks give reasona

ble descirptions to the ideal situationble descirptions to the ideal situation However, 16-AWS gives a relatively better resultHowever, 16-AWS gives a relatively better result

ResultsResults

Conclusion:Conclusion: Resonable estimate for idealiResonable estimate for idealizedzed microbursts microbursts

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Availability of the Real DataAvailability of the Real Data

Operation Period:Operation Period: 2727thth June 1998 to 26 June 1998 to 26thth October 1998 October 1998 a total of 122 daysa total of 122 days

Daily Data Monitoring is appliedDaily Data Monitoring is appliedData is collected in different time intervalsData is collected in different time intervals

BY1,3,5,6,7,8: every ONE secondBY1,3,5,6,7,8: every ONE second BY2,4 : every FIVE secondsBY2,4 : every FIVE seconds

Time averaging is used to remove high Time averaging is used to remove high frequency fluctuations with periods shorter frequency fluctuations with periods shorter than 1 minute (e.g. jet wash)than 1 minute (e.g. jet wash)

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ONE minute

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Case SelectionCase Selection

All data was averaged by every minuteAll data was averaged by every minuteGWD is found in each minuteGWD is found in each minuteCriteria for case study:Criteria for case study:

Failure PeriodsFailure Periods Testing PeriodsTesting Periods Thunderstorm and rainy DaysThunderstorm and rainy Days High wind speed PeriodsHigh wind speed Periods

METAR information is usedMETAR information is used

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Case SelectionCase Selection

CaseCase DateDate METAR info METAR info GWD GWD No. of No. of AWSAWS

II 07010701 TS, RA, 11 TS, RA, 11 8.10 8.10 55IIII 07120712 TS, RA, 7 TS, RA, 7 9.22 9.22 88IIIIII 07140714 TS, RA, 4 TS, RA, 4 7.74 7.74 88IVIV 07220722 N/A N/A 7.41 7.41 66VV 09110911 TS, RA, 5 TS, RA, 5 7.21 7.21 77VIVI 09130913 NIL, 5 NIL, 5 7.20 7.20 77VIIVII 10071007 NIL, 5 NIL, 5 11.3911.39 77VIIIVIII 10131013 NIL, 1 NIL, 1 9.68 9.68 77

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MethodologyMethodology

Divergence (DIV) along the runway is Divergence (DIV) along the runway is usedused

)()(21

)(DIV 11

iii xvxvx

Windshear is associated with a pair of Windshear is associated with a pair of convergence and divergence zonesconvergence and divergence zones

If the pair is moving, it is gust-front likeIf the pair is moving, it is gust-front likeIf the pair is nearly stationary, it is more If the pair is nearly stationary, it is more

likely a microburstlikely a microburst

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Case I: 980701Case I: 980701

14:40 15:20

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ResultsResults

There is a pair of There is a pair of movingmoving divergence and divergence and convergence zones from 14:52 to 15:00convergence zones from 14:52 to 15:00

It had gust-front featuresIt had gust-front featuresFigures about this caseFigures about this case

GWD GWD 8.10 m/s 8.10 m/s Length of Gust Length of Gust 195.65 m 195.65 m Duration Duration 10 minutes 10 minutes Skew angle Skew angle 10.49° 10.49°

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Case VII: 981007Case VII: 981007

02:30 03:00

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ResultsResults

There is a pair of There is a pair of nearly stationarynearly stationary divergence and convergence zonesdivergence and convergence zones

It had microburst featuresIt had microburst featuresFigures about this caseFigures about this case

GWD GWD 11.39 m/s 11.39 m/s Radius of Microburst Radius of Microburst 1.5 km 1.5 km Duration Duration 8 minutes 8 minutes

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ConclusionsConclusionsOur mathematical model can describe and Our mathematical model can describe and

detect the occurrence of windshear in both detect the occurrence of windshear in both idealized and real casesidealized and real cases

It registers a few cases of interesting It registers a few cases of interesting meteorological phenomena which had meteorological phenomena which had similar (but weaker) characteristicssimilar (but weaker) characteristics

Its setup price is relatively cheap, but it is Its setup price is relatively cheap, but it is reliable and easy to installreliable and easy to install

A denser AWS network (with more A denser AWS network (with more AWS) can improve the skill of the systemAWS) can improve the skill of the system

It is suitable detecting windshear for It is suitable detecting windshear for airports in the Asia-Pacific Regionairports in the Asia-Pacific Region

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AcknowledgementsAcknowledgements

Department of Mathematics, HKUSTDepartment of Mathematics, HKUSTCivil Aviation Administration of China Civil Aviation Administration of China

(CAAC)(CAAC)Center for Coastal and Atmospheric Center for Coastal and Atmospheric

Research (CCAR), HKUSTResearch (CCAR), HKUST''Operational Windshear Warning System Operational Windshear Warning System

(OWWS)' consultancy project(OWWS)' consultancy projectYour participationYour participation

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Thank YouThank You