Lecture # 05: Airfoil Wake Measurements and Calibration of a Hotwire Anemometer

Size: px
Start display at page:

Download "Lecture # 05: Airfoil Wake Measurements and Calibration of a Hotwire Anemometer"

Transcription

1 AerE L AerEL Lecture Notes Lecture # 5: Airfoil Wake Measureets ad Calibratio of a Hotwire Aeoeter r. Hui H Hu eartet of Aerosace Egieerig Iowa State iversit Aes, Iowa 5,.S.A Coright b r. Hui Iowa State iversit. All Rights Reserved!

2 Objectives of AerELL Objectives of the aerodaic lab courses:. To hel studets to gras cocets ad fudaetal riciles taught i aerodaics courses.. To rovide studets ore chaces to get hads-o lab exerieces.. To teach studets basic kowledge related to exerietal aerodaics ad easureets techiques.. To irove studets caabilities i egieerig writig b writig lab reorts. 5. To roote the sirit of tea-work aog the egieerig studets. Coright b r. Hui Iowa State iversit. All Rights Reserved!

3 AerELAerEL Gro ivisio Over 9 studets divided ito 6 lab sectios gros er sectio ~5 studets er gro Lab liitatios: ol oe set of exerietal facilit oe wid tuel oe test odel Studets colais ad cocers: TAs re-lab lecture is too log TAs will tr to fiish the exlaatio withi iutes Waitig tie is too log, ca we have gros/sectio ~8 studets er gro istead of gros/sectios ~5 studets er gro? eeds o the oiios of ajorit of the studets Coright b r. Hui Iowa State iversit. All Rights Reserved!

4 Lab : Airfoil Wake Measureets ad Hotwire Aeoeter Calibratio io Estiatios of the lift ad drag coefficiets of a airfoil Method : airfoil surface ressure easureets: Y iches X iches NACA airfoil er surface lower surface -.5 C x / c Coright b r. Hui Iowa State iversit. All Rights Reserved!

5 Lab : Airfoil Wake Measureets ad Hotwire Aeoeter Calibratio io Method : airfoil wake easureets: t C d ˆ CS F x For stead flow: d t C CS ˆ ˆ ˆ Coright b r. Hui Iowa State iversit. All Rights Reserved!

6 Coright Coright b r. Hui Iowa State iversit. All Rights Reserved! b r. Hui Iowa State iversit. All Rights Reserved! x Sice boudar ad is far awa fro the airfoil: Sice boudar ad is far awa fro the airfoil: ] ] ] ] ] ˆ ˆ ˆ ˆ ˆ CS Lab : Airfoil Wake Measureets ad Hotwire Aeoeter Calibrat Lab : Airfoil Wake Measureets ad Hotwire Aeoeter Calibratio io ˆ ; ˆ ˆ ˆ Coservatio of ass: Coservatio of ass: ] ˆ d t CS C r

7 Coright Coright b r. Hui Iowa State iversit. All Rights Reserved! b r. Hui Iowa State iversit. All Rights Reserved! x Lab : Airfoil Wake Measureets ad Hotwire Aeoeter Calibrat Lab : Airfoil Wake Measureets ad Hotwire Aeoeter Calibratio io ; ] ] Sice ˆ F F F X X CS X X ] ] d C C C C C Coared with the drag coefficiets obtaied based o airfoil s Coared with the drag coefficiets obtaied based o airfoil surface urface ressure easureets lab# at the sae agles of attack! ressure easureets lab# at the sae agles of attack!

8 Lab : Airfoil Wake Measureets ad Hotwire Aeoeter Calibratio io Pressure rake with total ressure robes the distace betwee the robes d x 8 Coright b r. Hui Iowa State iversit. All Rights Reserved!

9 Lab : Airfoil Wake Measureets ad Hotwire Aeoeter Calibratio io Flow Field Curret flow through wire c dt dt w i R w q Costat-teerature teerature aeoetr, T w CTA hotwire robe Coright b r. Hui Iowa State iversit. All Rights Reserved!

10 Hotwire Aeoeter Calibratio To quatif the relatioshi betwee the flow velocit ad voltage outut fro the CTA robe Flow velocit /s abxcx d*x e*x ax dev:.66, r. a.8, b.77, c-6.6, d. Curve fittig Exerietal data voltage Coright b r. Hui Iowa State iversit. All Rights Reserved!

AerE 343L: Aerodynamics Laboratory II. Lab Instructions

AerE 343L: Aerodynamics Laboratory II. Lab Instructions AerE 343L: Aerodynamics Laboratory II Lab Instructions Lab #2: Airfoil Pressure Distribution Measurements and Calibration of a Small Wind Tunnel Instructor: Dr. Hui Hu Department of Aerospace Engineering

More information

Lecture # 08: Boundary Layer Flows and Drag

Lecture # 08: Boundary Layer Flows and Drag AerE 311L & AerE343L Lecture Notes Lecture # 8: Boundary Layer Flows and Drag Dr. Hui H Hu Department of Aerospace Engineering Iowa State University Ames, Iowa 511, U.S.A y AerE343L #4: Hot wire measurements

More information

Lecture # 08: Boundary Layer Flows and Controls

Lecture # 08: Boundary Layer Flows and Controls AerE 344 Lecture Notes Lecture # 8: Boundary Layer Flows and Controls Dr. Hui Hu Department of Aerospace Engineering Iowa State University Ames, Iowa 511, U.S.A Flow Separation on an Airfoil Quantification

More information

25k June 2014

25k June 2014 o c. e g e l l a h c o i u d a r g. w ww 25k 28-29 Jue 214 k k 5 1 28-29 Jue 214 Walk it, Jog it, or Ru it - a NEW edurace challege alog a historic route. It s 1 k, 5 k, or 25 k o the Grad Uio Caal towpath,

More information

Lecture # 15: Aircraft and wind turbine icing and anti-/de-icing

Lecture # 15: Aircraft and wind turbine icing and anti-/de-icing AerE 344 Lecture Notes Lecture # 15: Aircraft and wind turbine icing and anti-/de-icing Dr Hui Hu Dr Rye M Waldman Department of Aerospace Engineering, Iowa State University Ames, Iowa 50011, U.S.A Introduction

More information

Polynomial functions have graphs that are smooth and continuous. c) Use your knowledge of quadratic functions to sketch the graph.

Polynomial functions have graphs that are smooth and continuous. c) Use your knowledge of quadratic functions to sketch the graph. Math 165 4.1 Polyomial fuctios I class work Polyomial fuctios have graphs that are smooth ad cotiuous 1) For the fuctio: y 2 = x 9. a) Write the fuctio i factored form. b) Fid the x-itercepts or real zeros

More information

.grandunionchallenge.com www 100km, 50km or 25km! June 2015

.grandunionchallenge.com www 100km, 50km or 25km! June 2015 o c. e g lle a h c io u d a r www.g! k 5 2 r o k 0 5, 100k 27-28 Jue 2015 27-28 Jue 2015 Walk it, Jog it, or Ru it - a edurace challege alog a historic route. It s 100k, 50k, or 25k o the Grad Uio Caal

More information

Computer Architecture ELEC3441

Computer Architecture ELEC3441 Computer rchitecture ELEC344 ISC vs CISC Iro Law CPUTime = # of istructio program # of cycle istructio cycle Lecture 5 Pipeliig () Dr. Hayde Kwok-Hay So Departmet of Electrical ad Electroic Egieerig L4

More information

THE EFFECTS OF COUPLED INDUCTORS IN PARALLEL INTERLEAVED BUCK CONVERTERS

THE EFFECTS OF COUPLED INDUCTORS IN PARALLEL INTERLEAVED BUCK CONVERTERS THE EFFECTS OF COUPED INDUCTORS IN PARAE INTEREAVED BUCK CONVERTERS Paul Seria, David Fi ad Geoff Walker pseria@itee.uq.edu.au School of Iformatio Techology ad Electrical Egieerig Uiversity of Queeslad

More information

Australian Journal of Basic and Applied Sciences. Rules Of Similarity For Model With Prototype Vertical Axis Wind Turbine

Australian Journal of Basic and Applied Sciences. Rules Of Similarity For Model With Prototype Vertical Axis Wind Turbine Australian Journal of Basic and Alied Sciences, 8(10) July 014, Pages: 309-315 AENSI Journals Australian Journal of Basic and Alied Sciences ISSN:1991-8178 Journal hoe age: www.ajbasweb.co Rules Of Siilarity

More information

8.5. Solving Equations II. Goal Solve equations by balancing.

8.5. Solving Equations II. Goal Solve equations by balancing. 8.5 Solvig Equatios II Goal Solve equatios by balacig. STUDENT BOOK PAGES 268 271 Direct Istructio Prerequisite Skills/Cocepts Solve a equatio by ispectio or systematic trial. Perform operatios usig itegers,

More information

C-1: Aerodynamics of Airfoils 1 C-2: Aerodynamics of Airfoils 2 C-3: Panel Methods C-4: Thin Airfoil Theory

C-1: Aerodynamics of Airfoils 1 C-2: Aerodynamics of Airfoils 2 C-3: Panel Methods C-4: Thin Airfoil Theory ROAD MAP... AE301 Aerodynamics I UNIT C: 2-D Airfoils C-1: Aerodynamics of Airfoils 1 C-2: Aerodynamics of Airfoils 2 C-3: Panel Methods C-4: Thin Airfoil Theory AE301 Aerodynamics I : List of Subjects

More information

SPH4U Transmission of Waves in One and Two Dimensions LoRusso

SPH4U Transmission of Waves in One and Two Dimensions LoRusso Waves travelig travellig from oe medium to aother will exhibit differet characteristics withi each medium. Rules A wave of fixed frequecy will have a shorter wavelegth whe passig from a fast medium to

More information

WIND TUNNEL EXPERIMENT ON THE EFFECT OF WIND ON SMOKE EXHAUST SYSTEMS FOR A HIGH RISE BUILDING

WIND TUNNEL EXPERIMENT ON THE EFFECT OF WIND ON SMOKE EXHAUST SYSTEMS FOR A HIGH RISE BUILDING WIND TUNNEL EXPERIMENT ON THE EFFECT OF WIND ON SMOKE EXHAUST SYSTEMS FOR A HIGH RISE BUILDING K.C. Chug Mechaical Egieerig, Natioal Yuli Uiversity of Sciece ad Techology Touliu City, Yuli 4, Taiwa ABSTRACT

More information

Lecture # 15: Aircraft and wind turbine icing and anti-/de-icing

Lecture # 15: Aircraft and wind turbine icing and anti-/de-icing AerE 344 Lecture Notes Lecture # 15: Aircraft and wind turbine icing and anti-/de-icing Dr Hui Hu Department of Aerospace Engineering, Iowa State University Ames, Iowa 50011, U.S.A Introduction Ice accretion

More information

Modeling Near-Shore Currents Induced by Irregular Breaking Wave

Modeling Near-Shore Currents Induced by Irregular Breaking Wave Joural of Coastal Research Special Issue 5 5-5 Florida, USA ISS 79-8 Modelig ear-shore Currets Iduced b Irregular Breakig Wave Ju Tag, Yog-Mig She ad Lei Cui State Ke Laborator of Coastal ad Offshore Egieerig,

More information

Long Win s Educational Facilities for Fluid Mechanics

Long Win s Educational Facilities for Fluid Mechanics Since 1985 F luid mechanics is a science to study how fluids flow and how fluids act on objects. T he wind tunnel is a comprehensive, complete and substantial system for students to study fundamental and

More information

SPEED OF SOUND MEASUREMENTS IN GAS-MIXTURES AT VARYING COMPOSITION USING AN ULTRASONIC GAS FLOW METER WITH SILICON BASED TRANSDUCERS

SPEED OF SOUND MEASUREMENTS IN GAS-MIXTURES AT VARYING COMPOSITION USING AN ULTRASONIC GAS FLOW METER WITH SILICON BASED TRANSDUCERS SPEED OF SOUND MEASUREMENTS IN GAS-MIXTURES AT VARYING COMPOSITION USING AN ULTRASONIC GAS FLOW METER WITH SILICON BASED TRANSDUCERS Torbjör Löfqvist, Kęstutis Sokas, Jerker Delsig EISLAB, Departmet of

More information

Representing polynominals with DFT (Discrete Fourier Transform) and FFT (Fast Fourier Transform) Arne Andersson

Representing polynominals with DFT (Discrete Fourier Transform) and FFT (Fast Fourier Transform) Arne Andersson Represetig polyomils with DFT Discrete Fourier Trsform d FFT Fst Fourier Trsform Are Adersso Iformtiostekologi Polyomil A Emple: 4 Coefficiet represettio:,,,4 Poit-vlue represettio:,, 4 4... 4,,,7,, Istitutioe

More information

Call To Action. & bb b b b. w w. œ œ œ J. &b b b b b. œ œ œ. œ œ. œ œ œ. ? b b b b b 4. j œ. j œ Ó n. œ j. œ j œ œ Ó Œ. œ j Ó Œ j œœ œ Ó.

Call To Action. & bb b b b. w w. œ œ œ J. &b b b b b. œ œ œ. œ œ. œ œ œ. ? b b b b b 4. j œ. j œ Ó n. œ j. œ j œ œ Ó Œ. œ j Ó Œ j œœ œ Ó. Voice Piao q=132 Comissioed by the Australia Museum of Democracy (MoAD) Call To Actio 4 By Tim Bevitt 2017 q=132 & bb b b b4 w w J 4 6 &b b b b b &b b b b b 10 µ J E F w w b We Our live here i Aus-tral

More information

Part III: Airfoil Data. Philippe Giguère

Part III: Airfoil Data. Philippe Giguère Part III: Airfoil Data Philippe Giguère Former Graduate Research Assistant (now with GE Wind Energy) Department of Aerospace Engineering University of Illinois at Urbana-Champaign Steady-State Aerodynamics

More information

The structure of the Fibonacci numbers in the modular ring Z 5

The structure of the Fibonacci numbers in the modular ring Z 5 Notes o Number Theory ad Discrete Mathematics Vol. 19, 013, No. 1, 66 7 The structure of the iboacci umbers i the modular rig Z J. V. Leyedekkers 1 ad A. G. Shao 1 aculty of Sciece, The Uiversity of Sydey

More information

Introduction to Algorithms 6.046J/18.401J/SMA5503

Introduction to Algorithms 6.046J/18.401J/SMA5503 Itroductio to Algorithms 6.046J/8.40J/SMA5503 Lecture 4 Prof. Charles E. Leiserso Quicsort Proposed by C.A.R. Hoare i 962. Divide-ad-coquer algorithm. Sorts i place lie isertio sort, but ot lie merge sort.

More information

Footwork is the foundation for a skilled basketball player, involving moves

Footwork is the foundation for a skilled basketball player, involving moves The Complete Book of Offesive Basketball Drills Basic Footwork ad Cuts Drills 2 Equipmet 16 chairs (or less) Persoel The etire team Basic Footwork ad Cuts Drills Two coaches How to Ru the Drill Five feet

More information

Coal Pulveriser. Global Solutions

Coal Pulveriser. Global Solutions Coal Pulveriser. Global Solutios > Worm Gears > Gear Uits > Coupligs & Freewheels Global Coal Pulveriser Solutios Reold is a global egieerig group with over 130 years of experiece i the desig ad maufacture

More information

Avai 193 Fall 2016 Laboratory Greensheet

Avai 193 Fall 2016 Laboratory Greensheet Avai 193 Fall 2016 Laboratory Greensheet Lab Report 1 Title: Instrumentation Test Technique Research Process: Break into groups of 4 people. These groups will be the same for all of the experiments performed

More information

AC : A STUDENT PROJECT ON AIRFOIL PERFORMANCE

AC : A STUDENT PROJECT ON AIRFOIL PERFORMANCE AC 2007-78: A STUDENT PROJECT ON AIRFOIL PERFORMANCE John Matsson, Oral Roberts University O. JOHN E. MATSSON is an Associate Professor of Mechanical Engineering at Oral Roberts University in Tulsa, Oklahoma.

More information

Aerodynamic Analyses of Horizontal Axis Wind Turbine By Different Blade Airfoil Using Computer Program

Aerodynamic Analyses of Horizontal Axis Wind Turbine By Different Blade Airfoil Using Computer Program ISSN : 2250-3021 Aerodynamic Analyses of Horizontal Axis Wind Turbine By Different Blade Airfoil Using Computer Program ARVIND SINGH RATHORE 1, SIRAJ AHMED 2 1 (Department of Mechanical Engineering Maulana

More information

A Comparative Investigation of Reheat In Gas Turbine Cycles

A Comparative Investigation of Reheat In Gas Turbine Cycles Proceedigs of the Iteratioal Gas Turbie ogress 3 Tokyo November -7, 3 IGT3Tokyo TS-86 A omparative Ivestigatio of Reheat I Gas Turbie ycles K. Sarabchi Departmet of Mechaical egieerig Uiversity of Tabriz

More information

SIMULATION OF THE VESSEL TRAFFIC SCHEDULE IN THE STRAIT OF ISTANBUL

SIMULATION OF THE VESSEL TRAFFIC SCHEDULE IN THE STRAIT OF ISTANBUL SIMULATIO OF THE VESSEL TRAFFIC SCHEDULE I THE STRAIT OF ISTAUL Şiri Özlem (a, İlha Or (a, irur Özbaş (b (a oğaziçi Uiversity, Istabul (b Rutgers, The State Uiversity of ew Jersey (a siriozlem@yahoo.com,

More information

DFC NIST DIGITAL MASS FLOW CONTROLLERS. DFC with optional LCD readout PROG RS485. Programmable Mass Flow Controller with Digital Signal Processing

DFC NIST DIGITAL MASS FLOW CONTROLLERS. DFC with optional LCD readout PROG RS485. Programmable Mass Flow Controller with Digital Signal Processing Programmable Mass Flow Cotroller with Digital Sigal Processig Microprocessor drive digital flow cotrollers allow oe to program, record, ad aalyze flow rates of various gases with a computer via a RS-485

More information

1. Write down the ideal gas law and define all its variable and parameters. 2. Calculate the values and units of the ideal gas law constant R.

1. Write down the ideal gas law and define all its variable and parameters. 2. Calculate the values and units of the ideal gas law constant R. Ideal Gases Objectives:. Write dow the ideal gas law ad defie all its variable ad parameters.. Calculate the values ad uits of the ideal gas law costat R. 3. Calculate the value of oe variable,, T, or,

More information

SERIES FP4000 FLOW RATES TABLE B** RANGE MODEL RANGE MODEL SERIES FP2000 FLOW RATES TABLE A** RANGE MODEL RANGE MODEL

SERIES FP4000 FLOW RATES TABLE B** RANGE MODEL RANGE MODEL SERIES FP2000 FLOW RATES TABLE A** RANGE MODEL RANGE MODEL Data Sheet Field IT Variable Area Flowmeters Acrylic VA Flowmeter Series FP Easy to read Eglish or Metric Scales Water rages from 4CCM to 20GPM Air rages from 50 CCM to 4000 LPM Threaded brass iserts for

More information

n UL Listed and FM Approved for n Solenoid control n Quick pressure relief valve 73Q n Pressure sustaining & reducing valve 723

n UL Listed and FM Approved for n Solenoid control n Quick pressure relief valve 73Q n Pressure sustaining & reducing valve 723 Pressure Relief/Sustaiig Valve Prioritizig pressure zoes Esurig cotrolled pipelie fill-up Prevetig pipelie emptyig Pump overload & cavitatio protectio Safeguardig pump miimum flow Excessive lie pressure

More information

COZY AIRCRAFT FORUM Chris Esselstyn s COZY MKIV Blended Winglets. Marc J. Zeitlin July 31 st, :45 PM 2:15 PM Forum Tent 02 GAMA Pavilion

COZY AIRCRAFT FORUM Chris Esselstyn s COZY MKIV Blended Winglets. Marc J. Zeitlin July 31 st, :45 PM 2:15 PM Forum Tent 02 GAMA Pavilion COZY AIRCRAFT FORUM Chris Esselstyn s COZY MKIV Blended Winglets Marc J. Zeitlin July 31 st, 2009 1:45 PM 2:15 PM Forum Tent 02 GAMA Pavilion What Will I Talk About? Chris s Plane Desire / Plan Fabrication

More information

AERODYNAMICS I LECTURE 7 SELECTED TOPICS IN THE LOW-SPEED AERODYNAMICS

AERODYNAMICS I LECTURE 7 SELECTED TOPICS IN THE LOW-SPEED AERODYNAMICS LECTURE 7 SELECTED TOPICS IN THE LOW-SPEED AERODYNAMICS The sources of a graphical material used in this lecture are: [UA] D. McLean, Understanding Aerodynamics. Arguing from the Real Physics. Wiley, 2013.

More information

Catenary Analysis and Calculation Method of Track Rope of Cargo Cableway with Multiple Loads

Catenary Analysis and Calculation Method of Track Rope of Cargo Cableway with Multiple Loads MATEC Web of Cofereces 8, 01008 (016) DOI: 10.1051/ mateccof/016801008 DME 016 Cateary Aalysis ad Calculatio Method of Track Rope of Cargo Cableway with Multiple Loads Jia Qi a, Ju Che, Liag Qiao, Jiacheg

More information

EFFECTS OF ROTOR CONTAMINATION ON GYROPLANE FLIGHT PERFORMANCE

EFFECTS OF ROTOR CONTAMINATION ON GYROPLANE FLIGHT PERFORMANCE 41 st Europea otorcraft Forum 2015 EFFECTS OF OTO CONTAMINATION ON GYOLANE FLIGHT EFOMANCE Holger uda, Falk Sachs, Jörg Seewald, Claas-Hirik ohardt L (Germa Aerospace Ceter) Liliethalplatz 7, 38108 Brauschweig,

More information

ScienceDirect. Investigation of the aerodynamic characteristics of an aerofoil shaped fuselage UAV model

ScienceDirect. Investigation of the aerodynamic characteristics of an aerofoil shaped fuselage UAV model Available online at www.sciencedirect.com ScienceDirect Procedia Engineering 90 (2014 ) 225 231 10th International Conference on Mechanical Engineering, ICME 2013 Investigation of the aerodynamic characteristics

More information

The Real Thing?: Representing the Bullfight and Spain in Death in the Afternoon by Peter Messent

The Real Thing?: Representing the Bullfight and Spain in Death in the Afternoon by Peter Messent The Real Thig?: Represetig the Bullfight ad Spai i Death i the Afteroo by Peter Messet Hemigway does t give us the real thig i the book; istead he gives us his versio of it Phrase used several times (both

More information

University of Bristol - Explore Bristol Research. Publisher's PDF, also known as Version of record

University of Bristol - Explore Bristol Research. Publisher's PDF, also known as Version of record Liu, X., Azarpeyvand, M., & Joseph, P. (2015). On the acoustic and aerodynamic performance of serrated airfoils. Paper presented at The 22nd International Congress on Sound and Vibration, Florence, France.

More information

Current as of September 20, 2013 (red items are new entries since last TAAHC meeting)

Current as of September 20, 2013 (red items are new entries since last TAAHC meeting) Tag Allocatio ad Applicatio Hut Committee Topic List Reiitiated i December 0 Nevada Board of Wildlife Documet prit size 8/ x 4 of Category Applicatio Hut (A) Curret as of September 0, 0 (red items are

More information

Chap 2. Statistical Properties and Spectra of Sea Waves

Chap 2. Statistical Properties and Spectra of Sea Waves Cha. Statitical Proertie ad Sectra o Sea Wave. Radom Wave Proile ad Deiitio o Rereetative wave.. Satial Surace Form o Sea Wave Log-creted wave: Wave cret have a log etet well, eecially i hallow water Short-creted

More information

draft final report NGSIM Arterial-Lane Selection Mode Federal Highway Administration Cambridge Systematics, Inc.

draft final report NGSIM Arterial-Lane Selection Mode Federal Highway Administration Cambridge Systematics, Inc. NGSIM Arterial-Lae Selectio Mode draft fial report prepared for Federal Highway Admiistratio prepared by Cambridge Systematics, Ic. with Itelliget Trasportatio Systems Laboratory Massachusetts Istitute

More information

OUTLINE FOR Chapter 4

OUTLINE FOR Chapter 4 16/8/3 OUTLINE FOR Chapter AIRFOIL NOMENCLATURE The leaing ege circle: (usually raius =. chor length c) The trailing ege: The chor line: Straight line connecting the center of leaing ege circle an the

More information

Research and Development Concerning Advancement of Composite Product by Injection in Mold Improvement of Interfacial Adhesion Performance

Research and Development Concerning Advancement of Composite Product by Injection in Mold Improvement of Interfacial Adhesion Performance *1) *1) *1) *2) *3) *4) *4) *4) *5) *5) *5) *6) *6) *6) Research ad Developmet Cocerig Advacemet of Composite Product by Ijectio i Mold Improvemet of Iterfacial Adhesio Performace MIKI Yasuhiro *1), NAKAI

More information

STUDY OF VARIOUS NACA SERIES AEROFOIL SECTIONS AND WING CONTOUR GENERATION USING CATIA V5

STUDY OF VARIOUS NACA SERIES AEROFOIL SECTIONS AND WING CONTOUR GENERATION USING CATIA V5 STUDY OF VARIOUS NACA SERIES AEROFOIL SECTIONS AND WING CONTOUR GENERATION USING CATIA V5 Pawan Kumar Department of Aeronautical Engineering, Desh Bhagat University, Punjab, India ABSTRACT Aerofoil is

More information

Static Extended Trailing Edge for Lift Enhancement: Experimental and Computational Studies

Static Extended Trailing Edge for Lift Enhancement: Experimental and Computational Studies Static Extended Trailing Edge for Lift Enhancement: Experimental and Computational Studies T. Liu, J. Montefort, W. Liou Western Michigan University Kalamazoo, MI 49008 and Q. Shams NASA Langley Research

More information

ANALYSIS AND MODELING TIME HEADWAY DISTRIBUTIONS UNDER HEAVY TRAFFIC FLOW CONDITIONS IN THE URBAN HIGHWAYS: CASE OF ISFAHAN

ANALYSIS AND MODELING TIME HEADWAY DISTRIBUTIONS UNDER HEAVY TRAFFIC FLOW CONDITIONS IN THE URBAN HIGHWAYS: CASE OF ISFAHAN TRANSPORT ISSN 648-442 prit / ISSN 648-348 olie 2 Volume 26(4): 375 382 doi:.3846/648442.2.635694 ANALYSIS AND MODELING TIME HEADWAY DISTRIBUTIONS UNDER HEAVY TRAFFIC FLOW CONDITIONS IN THE URBAN HIGHWAYS:

More information

A RECIPE TO ESTIMATE AERODYNAMICS AND LOADS ON ICED ROTOR BLADES

A RECIPE TO ESTIMATE AERODYNAMICS AND LOADS ON ICED ROTOR BLADES A RECIPE TO ESTIMATE AERODYNAMICS AND LOADS ON ICED ROTOR BLADES Henry Seifert*, Frank Richert** * Deutsches Windenergie-Institut, Ebertstraße 96, D-638 Wilhelmshaven, Germany ** Institut für Flugmechanik,

More information

HEFAT th International Conference on Heat Transfer, Fluid Mechanics and Thermodynamics July 2012 Malta

HEFAT th International Conference on Heat Transfer, Fluid Mechanics and Thermodynamics July 2012 Malta HEFAT212 9 th International Conference on Heat Transfer, Fluid Mechanics and Thermodynamics 16 18 July 212 Malta AN EXPERIMENTAL STUDY OF SWEEP ANGLE EFFECTS ON THE TRANSITION POINT ON A 2D WING BY USING

More information

Incompressible Flow over Airfoils

Incompressible Flow over Airfoils Road map for Chap. 4 Incompressible Flow over Airfoils Aerodynamics 2015 fall - 1 - < 4.1 Introduction > Incompressible Flow over Airfoils Incompressible flow over airfoils Prandtl (20C 초 ) Airfoil (2D)

More information

Theory of Flight Aircraft Design and Construction. References: FTGU pages 9-14, 27

Theory of Flight Aircraft Design and Construction. References: FTGU pages 9-14, 27 Theory of Flight 6.01 Aircraft Design and Construction References: FTGU pages 9-14, 27 Main Teaching Points Parts of an Airplane Aircraft Construction Landing Gear Standard Terminology Definition The airplane

More information

ROAD MAP... D-1: Aerodynamics of 3-D Wings D-2: Boundary Layer and Viscous Effects D-3: XFLR (Aerodynamics Analysis Tool)

ROAD MAP... D-1: Aerodynamics of 3-D Wings D-2: Boundary Layer and Viscous Effects D-3: XFLR (Aerodynamics Analysis Tool) Unit D-1: Aerodynamics of 3-D Wings Page 1 of 5 AE301 Aerodynamics I UNIT D: Applied Aerodynamics ROAD MAP... D-1: Aerodynamics of 3-D Wings D-: Boundary Layer and Viscous Effects D-3: XFLR (Aerodynamics

More information

ANALYSIS OF TRANSONIC FLOW OVER SUPERCRITICAL AIRFOIL USING CFD FOR GAS TURBINE BLADES

ANALYSIS OF TRANSONIC FLOW OVER SUPERCRITICAL AIRFOIL USING CFD FOR GAS TURBINE BLADES ANALYSIS OF TRANSONIC FLOW OVER SUPERCRITICAL AIRFOIL USING CFD FOR GAS TURBINE BLADES Kushal Gandecha 1 and Kalpit P. Kaurase 2 Abstract 1 Department of Mechanical Engineering, School of Engineering and

More information

ACKNOWLEDGEMENTS. My husband, Mr Matthew Pegg, for bearing with my non-stop complaints and long hours of work.

ACKNOWLEDGEMENTS. My husband, Mr Matthew Pegg, for bearing with my non-stop complaints and long hours of work. ABSTRACT This thesis describes the developmet, fudametal extesio ad extesive testig (validatio ad verificatio) of mathematical models for predictig outflow followig the failure of pressurised pipelies

More information

On the Relations between Lucas Sequence and Fibonacci-like Sequence by Matrix Methods

On the Relations between Lucas Sequence and Fibonacci-like Sequence by Matrix Methods .J. Mathematical Sciece ad Comutig, 07,, 0-36 Publihed Olie November 07 i MECS (htt://www.mec-re.et) DO: 0.8/ijmc.07.0.03 Available olie at htt://www.mec-re.et/ijmc O the Relatio betwee uca Sequece ad

More information

EMSBS/EMST. Drill For Machining Ultra-Deep Minute Holes FEATURES. For ultra-deep drilling of miniature holes. New chip stopper controls chip flow.

EMSBS/EMST. Drill For Machining Ultra-Deep Minute Holes FEATURES. For ultra-deep drilling of miniature holes. New chip stopper controls chip flow. EMSBS/EMST Drill For Machiig Ultra-Deep Miute Holes FEATURES For ultra-deep drillig of miiature holes. New chip stopper cotrols chip flow. EMSBS: Deep hole mirco-drills with TH Coatig. EMST: Micro- starter

More information

The Application of Simulating WAves Nearshore Model for Wave Height Simulation at Bangkhuntien Shoreline

The Application of Simulating WAves Nearshore Model for Wave Height Simulation at Bangkhuntien Shoreline America Joural of Evirometal Scieces 6 (3): 299-307, 2010 ISSN 1553-345X 2010 Sciece Publicatios The Applicatio of Simulatig WAves Nearshore Model for Wave Height Simulatio at Bagkhutie Shorelie 1 Prasertsak

More information

Measurement of Pressure. The aerofoil shape used in wing is to. Distribution and Lift for an Aerofoil. generate lift due to the difference

Measurement of Pressure. The aerofoil shape used in wing is to. Distribution and Lift for an Aerofoil. generate lift due to the difference Measurement of Pressure Distribution and Lift for an Aerofoil. Objective The objective of this experiment is to investigate the pressure distribution around the surface of aerofoil NACA 4415 and to determine

More information

What happens to a fluid (water or air) when it moves from entering a wide opening to entering a narrow opening?

What happens to a fluid (water or air) when it moves from entering a wide opening to entering a narrow opening? What happens to a fluid (water or air) when it moves from entering a wide opening to entering a narrow opening? The water (or air) speeds up. Since the same amount of water/air has to travel through a

More information

Basics of Flow measurement using Hot-film anemometer

Basics of Flow measurement using Hot-film anemometer Basics of Flow easureent using Hot-fil aneoeter Version 1.0 1/9 Inhaltsverzeichnis: 1. Definitions 1.1. Air Velocity 1.2. Aount (of Gas) 1.. Flow 1..1. Mass flow rate 1..2. Voluetric flow rate 1... Standard

More information

J. Szantyr Lecture No. 21 Aerodynamics of the lifting foils Lifting foils are important parts of many products of contemporary technology.

J. Szantyr Lecture No. 21 Aerodynamics of the lifting foils Lifting foils are important parts of many products of contemporary technology. J. Szantyr Lecture No. 21 Aerodynamics of the lifting foils Lifting foils are important parts of many products of contemporary technology. < Helicopters Aircraft Gliders Sails > < Keels and rudders Hydrofoils

More information

XFM DIGITAL MASS FLOW METER. XFM with Profibus Interface. XFM without. Readout. XFM with. Readout. Option

XFM DIGITAL MASS FLOW METER. XFM with Profibus Interface. XFM without. Readout. XFM with. Readout. Option BULLETIN EM20180402 Desig Features Supports up to 23 Egieerig Uits (icludig User Defied). Stores calibratio data for up to 10 gases. Programmable Totalizer idicates total gas quatity. High ad low gas flow

More information

Capacity of Shared-Short Lanes at Unsignalised Intersections

Capacity of Shared-Short Lanes at Unsignalised Intersections Nig Wu itle ad Abstract Author's Address apacity of Shared-Short aes at Usigalised Itersectios Nig Wu ABSA he calculatio procedures i recet highway capacity mauals do ot eactly treat ared/ort laes at usigalized

More information

CFD ANALYSIS OF FLOW AROUND AEROFOIL FOR DIFFERENT ANGLE OF ATTACKS

CFD ANALYSIS OF FLOW AROUND AEROFOIL FOR DIFFERENT ANGLE OF ATTACKS www.mechieprojects.com CFD ANALYSIS OF FLOW AROUND AEROFOIL FOR DIFFERENT ANGLE OF ATTACKS PRESENTATION OUTLINE AIM INTRODUCTION LITERATURE SURVEY CFD ANALYSIS OF AEROFOIL RESULTS CONCLUSIONS www.mechieprojects.com

More information

Activity Parts of an Aircraft

Activity Parts of an Aircraft Activity 4.2.7 Parts of an Aircraft Introduction The science of aeronautics really began to evolve in the late 18th and early 19th centuries. Philosophers and early scientists began to look closely at

More information

S L G. Chapter 12: The Behavior of Gases. I. First Concepts a. The 3 states of matter most important to us: solids, liquids, and gases.

S L G. Chapter 12: The Behavior of Gases. I. First Concepts a. The 3 states of matter most important to us: solids, liquids, and gases. Chapter : he ehaior of Gases I. First Concepts a. he 3 states of atter ost iportant to us: solids, liquids, and gases. S L G b. Real Gases and Ideal Gases i. Real gases exist, ideal gases do not ii. Under

More information

Wind Tunnel Tests of Wind Turbine Airfoils at High Reynolds Numbers

Wind Tunnel Tests of Wind Turbine Airfoils at High Reynolds Numbers Journal of Physics: Conference Series OPEN ACCESS Wind Tunnel Tests of Wind Turbine Airfoils at High Reynolds Numbers To cite this article: E Llorente et al 014 J. Phys.: Conf. Ser. 54 0101 View the article

More information

P h o t o g r a p h i c L i g h t i n g ( 1 1 B )

P h o t o g r a p h i c L i g h t i n g ( 1 1 B ) 9 1 5 9 P h o t o g r a p h i c L i g h t i g ( 1 1 B ) 30S/30E/30M A Photography Course 9 1 5 9 : P h o t o g r a p h i c L i g h t i g ( 1 1 B ) 3 0 S / 3 0 E / 3 0 M Course Descriptio This course focuses

More information

Mischa Salkind-Pearl Oceans:

Mischa Salkind-Pearl Oceans: Mischa Salkid-Pearl Oceas: waves merge with the bright sky or Masaki Hasebe ive cellos Perormace Istructios: Accidetals: There are several quarter-toe ad microtoal accidetals used i this score. They are

More information

Aerodynamic Forces on a Wing in a Subsonic Wind Tunnel. Learning Objectives

Aerodynamic Forces on a Wing in a Subsonic Wind Tunnel. Learning Objectives Aerodynamic Forces on a Wing in a Subsonic Wind Tunnel AerodynamicForces Lab -1 Learning Objectives 1. Familiarization with aerodynamic forces 2. Introduction to airfoil/wing basics 3. Use and operation

More information

number in a data set adds (or subtracts) that value to measures of center but does not affect measures of spread.

number in a data set adds (or subtracts) that value to measures of center but does not affect measures of spread. Lesso 3-3 Lesso 3-3 Traslatios of Data Vocabulary ivariat BIG IDEA Addig (or subtractig) the same value to every umber i a data set adds (or subtracts) that value to measures of ceter but does ot affect

More information

A Different View on TBM Face Equilibrium in Permeable Ground

A Different View on TBM Face Equilibrium in Permeable Ground A Differet View o TBM Face Equilibrium i Permeable Groud Tiago Gerheim Souza Dias Ghet Uiversity, Ghet, Belgium Adam Bezuije Ghet Uiversity, Ghet, Belgium ad Deltares, Delft, the Netherlads ABSTACT The

More information

WESEP 594 Research Seminar

WESEP 594 Research Seminar WESEP 594 Research Seminar Aaron J Rosenberg Department of Aerospace Engineering Iowa State University Major: WESEP Co-major: Aerospace Engineering Motivation Increase Wind Energy Capture Betz limit: 59.3%

More information

A SECOND SOLUTION FOR THE RHIND PAPYRUS UNIT FRACTION DECOMPOSITIONS

A SECOND SOLUTION FOR THE RHIND PAPYRUS UNIT FRACTION DECOMPOSITIONS Fudametal Joural of Mathematics ad Mathematical Scieces Vol., Issue, 0, Pages -55 This paper is available olie at http://www.frdit.com/ Published olie November 9, 0 A SECOND SOLUTION FOR THE RHIND PAPYRUS

More information

ASSESSMENT SCORING SYSTEM OF ROAD SAFETY INFRASTRUCTURE

ASSESSMENT SCORING SYSTEM OF ROAD SAFETY INFRASTRUCTURE ASSESSMENT SCORING SYSTEM OF ROAD SAFETY INFRASTRUCTURE Case Study of Mihag District i Shaghai, Chia Yue Wag, Daocheg Su 2 School of Traffic ad Trasportatio Egieerig, Togi Uiversity, Shaghai, Chia ABSTRACT

More information

Vessel Interaction A Case Study Peter O Brien, Dr Terry O Brien, Chris Hens OMC International Pty Ltd, Melbourne, Australia

Vessel Interaction A Case Study Peter O Brien, Dr Terry O Brien, Chris Hens OMC International Pty Ltd, Melbourne, Australia Vessel Interaction A Case Study eter O Brien, Dr Terry O Brien, Chris Hens OMC International ty Ltd, Melbourne, Australia Abstract The growth in vessel sizes is lacing orts under increasing ressure to

More information

Application of Low Speed Wind Tunnels in Teaching Basic Aerodynamics

Application of Low Speed Wind Tunnels in Teaching Basic Aerodynamics Journal of Aviation/Aerospace Education & Research Volume 14 Number 2 JAAER Winter 2005 Article 6 Winter 2005 Application of in Teaching Basic Aerodynamics Randolph S. Reynolds Follow this and additional

More information

AE Dept., KFUPM. Dr. Abdullah M. Al-Garni. Fuel Economy. Emissions Maximum Speed Acceleration Directional Stability Stability.

AE Dept., KFUPM. Dr. Abdullah M. Al-Garni. Fuel Economy. Emissions Maximum Speed Acceleration Directional Stability Stability. Aerodynamics: Introduction Aerodynamics deals with the motion of objects in air. These objects can be airplanes, missiles or road vehicles. The Table below summarizes the aspects of vehicle performance

More information

OBJECTIVE METHODOLOGY

OBJECTIVE METHODOLOGY SKMA394 Measurement of Pressure Distribution around an Airfoil NACA445 OBJECTIVE The objective of this experiment is to study about the pressure distribution around the surface of aerofoil NACA 445 starting

More information

Influences of Teaching Styles and Motor Educability on Learning Outcomes of Volleyball

Influences of Teaching Styles and Motor Educability on Learning Outcomes of Volleyball Asia Social Sciece; Vol., No. 5; 14 ISSN 1911-17 E-ISSN 1911-5 Published by Caadia Ceter of Sciece ad Educatio Iflueces of Teachig Styles ad Motor Educability o Learig Outcomes of Volleyball Syamsuddi

More information

Load Calculation and Design of Roller Crowning of Truck Hub Bearing

Load Calculation and Design of Roller Crowning of Truck Hub Bearing Sed Orders for Reprits to reprits@bethamsciece.ae 106 The Ope Mechaical Egieerig Joural, 2015, 9, 106-110 Ope Access Load Calculatio ad Desig of Roller Crowig of Truck Hub Bearig Xitao Xia,1, Shujig Dog

More information

Status Report on IEICE Communications Society (IEICE-CS)

Status Report on IEICE Communications Society (IEICE-CS) Status Report o IEICE Commuicatios Society (IEICE-CS) http://www.ieice.org/cs/idex.html 2017 IEICE. All Rights Reserved About IEICE 1917 established 1995 5 societies + 1 group 2016 Egieerig Scieces Society(ESS)

More information

Overview. Creating Walkable, Bikeable Communities Developing Effective Active Transportation Projects and Programs. Add photo or photos

Overview. Creating Walkable, Bikeable Communities Developing Effective Active Transportation Projects and Programs. Add photo or photos Creatig Walkable, Bikeable Commuities Developig Effective Active Trasportatio Projects ad Programs Add photo or photos Sposored by Caltras ad [local sposors] Overview Effective itervetios that ca improve

More information

CFD AND EXPERIMENTAL STUDY OF AERODYNAMIC DEGRADATION OF ICED AIRFOILS

CFD AND EXPERIMENTAL STUDY OF AERODYNAMIC DEGRADATION OF ICED AIRFOILS Colloquium FLUID DYNAMICS 2008 Institute of Thermomechanics AS CR, v.v.i., Prague, October 22-24, 2008 p.1 CFD AND EXPERIMENTAL STUDY OF AERODYNAMIC DEGRADATION OF ICED AIRFOILS Vladimír Horák 1, Dalibor

More information

Projectile Motion Lab (2019)

Projectile Motion Lab (2019) Nae: Date: Partner(s): Period: Projectile Motion Lab (2019) Object: Measure the velocity of a ball using two Photogates and coputer software for tiing. Apply concepts fro two-diensional kineatics to predict

More information

AN EXPERIMENTAL STUDY OF THE EFFECTS OF SWEPT ANGLE ON THE BOUNDARY LAYER OF THE 2D WING

AN EXPERIMENTAL STUDY OF THE EFFECTS OF SWEPT ANGLE ON THE BOUNDARY LAYER OF THE 2D WING AN EXPERIMENTAL STUDY OF THE EFFECTS OF SWEPT ANGLE ON THE BOUNDARY LAYER OF THE 2D WING A. Davari *, M.R. Soltani, A.Tabrizian, M.Masdari * Assistant Professor, Department of mechanics and Aerospace Engineering,

More information

THE LATENT DEMAND METHOD

THE LATENT DEMAND METHOD THE LATENT DEMAND METHOD Bruce W. Ladis, Russell M. Otteberg, Vekat R. Vattikuti SCI, Ic., 18115 U.S. Highway 41North, Suite 600, Lutz, FL 33549, USA Email: bladis@sciworld.et Travel patters i a metropolita

More information

The Complete Book of Offensive. Basketball Drills GAME-CHANGING DRILLS FROM AROUND THE WORLD GIORGIO GANDOLFI

The Complete Book of Offensive. Basketball Drills GAME-CHANGING DRILLS FROM AROUND THE WORLD GIORGIO GANDOLFI The Complete Book of Offesive Basketball Drills GAME-CHANGING DRILLS FROM AROUND THE WORLD GIORGIO GANDOLFI New York Chicago Sa Fracisco Lisbo Lodo Madrid Mexico City Mila New Delhi Sa Jua Seoul Sigapore

More information

Permutations and Combinations

Permutations and Combinations 13 Pemutatios ad Combiatios TERMINOLOGY Aagemets: Diffeet ways of ogaisig objects Combiatios: Aagemets of objects without eplacemet o epetitio whe ode is ot impotat. The otatio used is C fo selectig objects

More information

Numerical Simulation And Aerodynamic Performance Comparison Between Seagull Aerofoil and NACA 4412 Aerofoil under Low-Reynolds 1

Numerical Simulation And Aerodynamic Performance Comparison Between Seagull Aerofoil and NACA 4412 Aerofoil under Low-Reynolds 1 Advances in Natural Science Vol. 3, No. 2, 2010, pp. 244-20 www.cscanada.net ISSN 171-7862 [PRINT] ISSN 171-7870 [ONLINE] www.cscanada.org *The 3rd International Conference of Bionic Engineering* Numerical

More information

CFD Study of Solid Wind Tunnel Wall Effects on Wing Characteristics

CFD Study of Solid Wind Tunnel Wall Effects on Wing Characteristics Indian Journal of Science and Technology, Vol 9(45), DOI :10.17485/ijst/2016/v9i45/104585, December 2016 ISSN (Print) : 0974-6846 ISSN (Online) : 0974-5645 CFD Study of Solid Wind Tunnel Wall Effects on

More information

GFC NIST MASS FLOW CONTROLLERS. Typical Stainless Steel GFC Mass Flow Controller. Design Features. General Description. Principles of Operation

GFC NIST MASS FLOW CONTROLLERS. Typical Stainless Steel GFC Mass Flow Controller. Design Features. General Description. Principles of Operation BULLETIN EM20180402 Model thermal Mass Flow Cotrollers are desiged to idicate ad cotrol set flow rates of gases. The combies the characteristics ad accuracy of covetioal mass flow devices ito a uique compact

More information

PASSIVE FLOW SEPARATION CONTROL BY STATIC EXTENDED TRAILING EDGE

PASSIVE FLOW SEPARATION CONTROL BY STATIC EXTENDED TRAILING EDGE Proceedings of the International Conference on Mechanical Engineering and Renewable Energy 25 (ICMERE25) 26 29 November, 25, Chittagong, Bangladesh ICMERE25-PI-232 PASSIVE FLOW SEPARATION CONTROL BY STATIC

More information

Patrick Boston (Leeds University) and Mark Chapman (Edinburgh University)

Patrick Boston (Leeds University) and Mark Chapman (Edinburgh University) Iversio o requecy-depedet AVO data or luid properties Patric Bosto (Leeds Uiversity) ad Mar Chapma (Ediburgh Uiversity) Summary A umber o methods to estimate the requecy-depedece o relectivity have bee

More information

Team Michigan Small Area Games Small Area Games. 6 Goal Scoring Games 4 Passing/Puck Control Games w/ no Goalies

Team Michigan Small Area Games   Small Area Games. 6 Goal Scoring Games 4 Passing/Puck Control Games w/ no Goalies 1 Small Area Games 6 Goal Scoring Games 4 Passing/Puck Control Games w/ no Goalies By Jeff Hatley USA Hockey Coaching Education Program Instructor Asst. Coach - Team Michigan March 17, 2005 Small Area

More information

GFC NIST MASS FLOW CONTROLLERS. Typical Stainless Steel GFC Mass Flow Controller. Design Features. General Description. Principles of Operation

GFC NIST MASS FLOW CONTROLLERS. Typical Stainless Steel GFC Mass Flow Controller. Design Features. General Description. Principles of Operation Model thermal Mass Flow Cotrollers are desiged to idicate ad cotrol set flow rates of gases. The combies the characteristics ad accuracy of covetioal mass flow devices ito a uique compact desig at low

More information

Computation of the inviscid drift force caused by nonlinear waves on a submerged circular cylinder

Computation of the inviscid drift force caused by nonlinear waves on a submerged circular cylinder csnak, 2011 Iter J Nav Archit Oc Egg (2011) 3:201~207 http://dx.doi.org/10.3744/jnaoe.2011.3.3.201 Computatio of the iviscid drift force caused by oliear waves o a submerged circular cylider Hyeok-Ju Koh

More information