ADVANCES IN AERODYNAMICS OF WIND TURBINE BLADES

Size: px
Start display at page:

Download "ADVANCES IN AERODYNAMICS OF WIND TURBINE BLADES"

Transcription

1 ADVANCES IN AERODYNAMICS OF WIND TURBINE BLADES Herning / October 3 / 2017 By Jesper Madsen Chief Engineer, Aerodynamics & Acoustics WIND ENERGY DENMARK Annual Event 2017

2 Agenda 1. Aerodynamic design and developments 2. Innovative tip designs 3. LM Vortex Generator Mk II 2

3 Aerodynamic blade design considerations 3

4 Aerodynamic Developments LM Serrations Focus areas: Low-Noise performance Blade design Devices Aerodynamic tailoring: Wide variation in LM-Airfoil characteristics covers requirements from small on-shore turbines to ultra-long offshore blades Blade optimization Leading Edge Erosion: Aerodynamic impact of eroded blade Erosion protection systems Devices LM T-Spoiler Serrations (acoustics) Vortex Generators T-spoiler (root performance) 4

5 Conventional Blade Tip Innovative Tip Designs Objectives: Reduction of Turbine Wake to improve total windfarm yield Optimize blade tip aerodynamics Reduction of Noise Turbulators ECN Patented Winglet

6 Tip Extension Field Installation and Testing Results: Increase in power output between 5% to 6% at wind speeds between 6 m/s and 9 m/s for conventional blade tip extension. Extending blade accounts for about 4% power increase remainder is optimization in shape.

7 LM Vortex Generator Mk II Continuous Improvement 7

8 Vortex generators improve blade performance by reducing flow separation Without VGs With VGs Low AoA Clean surface flow is separating VGs maintain attached flow Smooth airflow Vortex airflow Max. lift AoA Boundary layer separated Boundary layer attached Stall AoA Uncontrolled turbulence Controlled vortices Compared to a clean blade, VG s typically improves AEP by 0.5% 1% 8

9 LM Vortex Generators Mk II Mk II consists of a single vane on base plate Vanes are mounted on top of blade surface using a tape interface Panel-VG flush-mounted in groove OLD VG s are available in different sizes, so range of applications can be covered Bonding process is covered by international published patent application NEW Material changed to a tougher, more UV stable plastic 9

10 LM Vortex Generator s Mk II Single Fin VG design philosophy completely re-engineered Reliable performance predictions for wide range of airfoil thicknesses, VG configurations, combinations with other Add-Ons obtained from LM Wind tunnel tests Optimal and Robust VG design (geometry and configuration) understanding obtained from exhaustive wind tunnel testing MKII VG s Close up View Some Tested Geometries MKII VG s On an Airfoil in LM Wind Tunnel Performance coefficients from wind tunnel test 10

11 Experimental Optimization of VG Parameters Experimental results from LM Wind Power Low Speed Wind Tunnel (LM LSWT) measurements LM wind tunnel Objective: reduction in drag along with increased or same lift and delayed stall Parameters: Foot plate shape and thickness Chord wise placement Fin geometry Triangular Height (h) Length (l) Configuration: Spacing between pairs (z) Spacing between fins (s) Fin angle (β) Some results are presented in next slides 11

12 Effect of chord wise location VGs closer to the leading edge of the profile has highest increment in the Cl But the same time the increment in the Cd is also more 12

13 Effect of VG height VG with lower height performing better in terms of C lmax and AoA-C lmax and also drag h/c=2% is too high 13

14 Effect of VG spacing z/h=3 has highest increment in Cl (with more Cd) z/h=5 has high Cl/Cd ratio over wider AOA range z/h=7 has highest maximum Cl/Cd (also better than clean) 14

15 Automated Design Tools VG positioning on blade surface Several checks are built in: Aerodynamic force Centrifugal force Different sizes Blade surface curvature VG angle Mould Marks Etc. 15

16 LM Vortex Generator s Mk II Continuous Improvement project to improve the existing LM VG offering along with Improved Aerodynamics Improved Reliability Simplified and Robust installation process Enables service / retro-fit offerings Completely re-designed approach having single fins in an integrated mounting system with focusing on each of the above aspects Exhaustively Tested and Validated designs for performance 16

17 Thank you for your time Contact details: Head quarters: Jesper Madsen LM Wind Power Chief Engineer Jupitervej 6 Aerodynamics & Acoustics 6000 Kolding Denmark Tel Tel Mob Fax E jema@lmwindpower.com E info@lmwindpower.com W lmwindpower.com Note: The contents of this presentation are confidential and may not be copied, distributed, published or reproduced in whole or in part, or disclosed or distributed by recipients to any other person. 17

APPLICATION OF RESEARCH RESULTS AT LM WIND POWER

APPLICATION OF RESEARCH RESULTS AT LM WIND POWER APPLICATION OF RESEARCH RESULTS AT LM WIND POWER Herning / March 27 / 2014 By Jesper Madsen Chief Engineer Aerodynamics and Acoustics AGENDA 1. EUDP Projects 1. DANAERO MW 2. Optimization of vortex generators

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

PRESSURE DISTRIBUTION OF SMALL WIND TURBINE BLADE WITH WINGLETS ON ROTATING CONDITION USING WIND TUNNEL

PRESSURE DISTRIBUTION OF SMALL WIND TURBINE BLADE WITH WINGLETS ON ROTATING CONDITION USING WIND TUNNEL International Journal of Mechanical and Production Engineering Research and Development (IJMPERD ) ISSN 2249-6890 Vol.2, Issue 2 June 2012 1-10 TJPRC Pvt. Ltd., PRESSURE DISTRIBUTION OF SMALL WIND TURBINE

More information

Uncontrolled copy not subject to amendment. Principles of Flight

Uncontrolled copy not subject to amendment. Principles of Flight Uncontrolled copy not subject to amendment Principles of Flight Principles of Flight Learning Outcome 1: Know the principles of lift, weight, thrust and drag and how a balance of forces affects an aeroplane

More information

Aerodynamic Analysis of Blended Winglet for Low Speed Aircraft

Aerodynamic Analysis of Blended Winglet for Low Speed Aircraft , July 1-3, 2015, London, U.K. Aerodynamic Analysis of Blended Winglet for Low Speed Aircraft Pooja Pragati, Sudarsan Baskar Abstract This paper provides a practical design of a new concept of massive

More information

Part I: Blade Design Methods and Issues. James L. Tangler

Part I: Blade Design Methods and Issues. James L. Tangler Part I: Blade Design Methods and Issues James L. Tangler Senior Scientist National Renewable Energy Laboratory National Wind Technology Center Steady-State Aerodynamics Codes for HAWTs Selig, Tangler,

More information

Pressure distribution of rotating small wind turbine blades with winglet using wind tunnel

Pressure distribution of rotating small wind turbine blades with winglet using wind tunnel Journal of Scientific SARAVANAN & Industrial et al: Research PRESSURE DISTRIBUTION OF SMALL WIND TURBINE BLADES WITH WINGLET Vol. 71, June 01, pp. 45-49 45 Pressure distribution of rotating small wind

More information

NAWEA 2015 SYMPOSIUM

NAWEA 2015 SYMPOSIUM Aerodynamics and Aeroacoustics of Spanwise Wavy Trailing Edge Flatback Airfoils: Design Improvement Seung Joon Yang James D. Baeder Alfred Gessow Rotorcraft Center Department of Aerospace Engineering,

More information

EXPERIMENTAL INVESTIGATION OF LIFT & DRAG PERFORMANCE OF NACA0012 WIND TURBINE AEROFOIL

EXPERIMENTAL INVESTIGATION OF LIFT & DRAG PERFORMANCE OF NACA0012 WIND TURBINE AEROFOIL EXPERIMENTAL INVESTIGATION OF LIFT & DRAG PERFORMANCE OF NACA0012 WIND TURBINE AEROFOIL Mr. Sandesh K. Rasal 1, Mr. Rohan R. Katwate 2 1 PG Student, 2 Assistant Professor, DYPSOEA Ambi Talegaon, Heat Power

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

EFFECT OF GURNEY FLAPS AND WINGLETS ON THE PERFORMANCE OF THE HAWT

EFFECT OF GURNEY FLAPS AND WINGLETS ON THE PERFORMANCE OF THE HAWT Chapter-6 EFFECT OF GURNEY FLAPS AND WINGLETS ON THE PERFORMANCE OF THE HAWT 6.1 Introduction The gurney flap (wicker bill) was a small flat tab projecting from the trailing edge of a wing. Typically it

More information

Jet Propulsion. Lecture-17. Ujjwal K Saha, Ph. D. Department of Mechanical Engineering Indian Institute of Technology Guwahati

Jet Propulsion. Lecture-17. Ujjwal K Saha, Ph. D. Department of Mechanical Engineering Indian Institute of Technology Guwahati Lecture-17 Prepared under QIP-CD Cell Project Jet Propulsion Ujjwal K Saha, Ph. D. Department of Mechanical Engineering Indian Institute of Technology Guwahati 1 Lift: is used to support the weight of

More information

The effect of back spin on a table tennis ball moving in a viscous fluid.

The effect of back spin on a table tennis ball moving in a viscous fluid. How can planes fly? The phenomenon of lift can be produced in an ideal (non-viscous) fluid by the addition of a free vortex (circulation) around a cylinder in a rectilinear flow stream. This is known as

More information

(51) Int Cl.: F03D 1/06 ( )

(51) Int Cl.: F03D 1/06 ( ) (19) TEPZZ 68Z 4B_T (11) EP 2 368 034 B1 (12) EUROPEAN PATENT SPECIFICATION (4) Date of publication and mention of the grant of the patent: 28.06.17 Bulletin 17/26 (21) Application number: 09737464.9 (22)

More information

FLOW CONTROL APPLIED TO OUTER WING SLAT-EDGE PROBLEM: CFD & EXPERIMENT

FLOW CONTROL APPLIED TO OUTER WING SLAT-EDGE PROBLEM: CFD & EXPERIMENT FLOW CONTROL APPLIED TO OUTER WING SLAT-EDGE PROBLEM: CFD & EXPERIMENT IAP 30 March 2017 Tel-Aviv University (TAU) IAI: I. Detinis, M. Steinbuch, S. Segal TAU: M. Lagutin & A. Seifert This study is part

More information

Wind Turbine Noise Emission Customised Solutions for French Legislation

Wind Turbine Noise Emission Customised Solutions for French Legislation Wind Turbine Noise Emission Customised Solutions for French Legislation Énergie éolienne et innovation : quelles solutions face aux exigences techniques, réglementaires et environnementales? MEDDTL le

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

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

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

Computationally Efficient Determination of Long Term Extreme Out-of-Plane Loads for Offshore Turbines

Computationally Efficient Determination of Long Term Extreme Out-of-Plane Loads for Offshore Turbines Computationally Efficient Determination of Long Term Extreme Out-of-Plane Loads for Offshore Turbines Anand Natarajan Senior Scientist Wind Energy Department, Risø DTU Denmark Introduction IEC 61400-1

More information

Senior mechanical energy conversion trends

Senior mechanical energy conversion trends Senior mechanical energy conversion trends Introduction and Analysis to fan blade profile and CFD Simulation Of An Appropriate Blade Profile for improving energy efficiency HAMED ROSTAMALIZADEH 95742906

More information

Basic Fluid Mechanics

Basic Fluid Mechanics Basic Fluid Mechanics Chapter 7B: Forces on Submerged Bodies 7/26/2018 C7B: Forces on Submerged Bodies 1 Forces on Submerged Bodies Lift and Drag are forces exerted on an immersed body by the surrounding

More information

AERODYNAMIC CHARACTERISTICS OF NACA 0012 AIRFOIL SECTION AT DIFFERENT ANGLES OF ATTACK

AERODYNAMIC CHARACTERISTICS OF NACA 0012 AIRFOIL SECTION AT DIFFERENT ANGLES OF ATTACK AERODYNAMIC CHARACTERISTICS OF NACA 0012 AIRFOIL SECTION AT DIFFERENT ANGLES OF ATTACK SUPREETH NARASIMHAMURTHY GRADUATE STUDENT 1327291 Table of Contents 1) Introduction...1 2) Methodology.3 3) Results...5

More information

Improved Aerodynamic Characteristics of Aerofoil Shaped Fuselage than that of the Conventional Cylindrical Shaped Fuselage

Improved Aerodynamic Characteristics of Aerofoil Shaped Fuselage than that of the Conventional Cylindrical Shaped Fuselage International Journal of Scientific & Engineering Research Volume 4, Issue 1, January-213 1 Improved Aerodynamic Characteristics of Aerofoil Shaped Fuselage than that of the Conventional Cylindrical Shaped

More information

Computational Analysis of Blunt Trailing Edge NACA 0012 Airfoil

Computational Analysis of Blunt Trailing Edge NACA 0012 Airfoil Computational Analysis of Blunt Trailing Edge NACA 2 Airfoil Anusha K Department of Aerospace Engineering Madras Institute of Technology, India anusugan7@gmail.com Abstract Blunt trailing edge airfoil

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

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

BUILD AND TEST A WIND TUNNEL

BUILD AND TEST A WIND TUNNEL LAUNCHING INTO AVIATION 9 2018 Aircraft Owners and Pilots Association. All Rights Reserved. UNIT 2 SECTION D LESSON 2 PRESENTATION BUILD AND TEST A WIND TUNNEL LEARNING OBJECTIVES By the end of this lesson,

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

Low Speed Wind Tunnel Wing Performance

Low Speed Wind Tunnel Wing Performance Low Speed Wind Tunnel Wing Performance ARO 101L Introduction to Aeronautics Section 01 Group 13 20 November 2015 Aerospace Engineering Department California Polytechnic University, Pomona Team Leader:

More information

Computational studies on small wind turbine performance characteristics

Computational studies on small wind turbine performance characteristics Journal of Physics: Conference Series PAPER OPEN ACCESS Computational studies on small wind turbine performance characteristics To cite this article: N Karthikeyan and T Suthakar 2016 J. Phys.: Conf. Ser.

More information

Aerodynamic Performance Optimization Of Wind Turbine Blade By Using High Lifting Device

Aerodynamic Performance Optimization Of Wind Turbine Blade By Using High Lifting Device Aerodynamic Performance Optimization Of Wind Turbine Blade By Using High Lifting Device Razeen Ridhwan, Mohamed Alshaleeh, Arunvinthan S Abstract: In the Aerodynamic performance of wind turbine blade by

More information

5 th European Conference on Turbomaschinery - Fluid Dynamics and Thermodynamics in Prague in March 2003

5 th European Conference on Turbomaschinery - Fluid Dynamics and Thermodynamics in Prague in March 2003 5 th European Conference on Turbomaschinery - Fluid Dynamics and Thermodynamics in Prague in March 2003 Secondary flow control on compressor blades to improve the performance of axial turbomachines R.

More information

An Analysis of Lift and Drag Forces of NACA Airfoils Using Python

An Analysis of Lift and Drag Forces of NACA Airfoils Using Python An Analysis of Lift and Drag Forces of NACA Airfoils Using Python 1. Tarun B Patel, Sandip T Patel 2, Divyesh T Patel 3, Maulik Bhensdadiya 4 1 M E scholar Government Engineering College, Valsad, Gujarat,

More information

Comparing GU & Savier airfoil equipped half canard In S4 wind tunnel (France)

Comparing GU & Savier airfoil equipped half canard In S4 wind tunnel (France) Some notes about Comparing GU & Savier airfoil equipped half canard In S4 wind tunnel (France) Matthieu Scherrer Adapted from Charlie Pujo & Nicolas Gorius work Contents Test conditions 3. S-4 Wind-tunnel.............................................

More information

EXPERIMENTAL ANALYSIS OF FLOW OVER SYMMETRICAL AEROFOIL Mayank Pawar 1, Zankhan Sonara 2 1,2

EXPERIMENTAL ANALYSIS OF FLOW OVER SYMMETRICAL AEROFOIL Mayank Pawar 1, Zankhan Sonara 2 1,2 EXPERIMENTAL ANALYSIS OF FLOW OVER SYMMETRICAL AEROFOIL Mayank Pawar 1, Zankhan Sonara 2 1,2 Assistant Professor,Chandubhai S. Patel Institute of Technology, CHARUSAT, Changa, Gujarat, India Abstract The

More information

Reduction of Skin Friction Drag in Wings by Employing Riblets

Reduction of Skin Friction Drag in Wings by Employing Riblets Reduction of Skin Friction Drag in Wings by Employing Riblets Kousik Kumaar. R 1 Assistant Professor Department of Aeronautical Engineering Nehru Institute of Engineering and Technology Coimbatore, India

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

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

Aerodynamics of Winglet: A Computational Fluid Dynamics Study Using Fluent

Aerodynamics of Winglet: A Computational Fluid Dynamics Study Using Fluent Aerodynamics of : A Computational Fluid Dynamics Study Using Fluent Rohit Jain 1, Mr. Sandeep Jain, Mr. Lokesh Bajpai 1PG Student, Associate Professor, Professor & Head 1 Mechanical Engineering Department

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

Design of a family of new advanced airfoils for low wind class turbines

Design of a family of new advanced airfoils for low wind class turbines Journal of Physics: Conference Series OPEN ACCESS Design of a family of new advanced airfoils for low wind class turbines To cite this article: Francesco Grasso 2014 J. Phys.: Conf. Ser. 555 012044 View

More information

Evaluation of aerodynamic criteria in the design of a small wind turbine with the lifting line model

Evaluation of aerodynamic criteria in the design of a small wind turbine with the lifting line model Evaluation of aerodynamic criteria in the design of a small wind turbine with the lifting line model Nicolas BRUMIOUL Abstract This thesis deals with the optimization of the aerodynamic design of a small

More information

Computational Analysis of Cavity Effect over Aircraft Wing

Computational Analysis of Cavity Effect over Aircraft Wing World Engineering & Applied Sciences Journal 8 (): 104-110, 017 ISSN 079-04 IDOSI Publications, 017 DOI: 10.589/idosi.weasj.017.104.110 Computational Analysis of Cavity Effect over Aircraft Wing 1 P. Booma

More information

EFFECT OF VORTEX GENERATORS ON THE PERFORMANCE OF HAWT

EFFECT OF VORTEX GENERATORS ON THE PERFORMANCE OF HAWT Chapter-7 EFFECT OF VORTEX GENERATORS ON THE PERFORMANCE OF HAWT 7.1 Introduction The wind turbine is intended for transformation of wind energy into electrical or mechanical energy and can be used in

More information

A COMPUTATIONAL STUDY ON THE DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF THE VEHICLE

A COMPUTATIONAL STUDY ON THE DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF THE VEHICLE 28 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES A COMPUTATIONAL STUDY ON THE DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF THE VEHICLE Jung-Hyun Kim*, Kyu-Hong

More information

Incompressible Potential Flow. Panel Methods (3)

Incompressible Potential Flow. Panel Methods (3) Incompressible Potential Flow Panel Methods (3) Outline Some Potential Theory Derivation of the Integral Equation for the Potential Classic Panel Method Program PANEL Subsonic Airfoil Aerodynamics Issues

More information

CFD Studies on Triangular Micro-Vortex Generators in Flow Control

CFD Studies on Triangular Micro-Vortex Generators in Flow Control IOP Conference Series: Materials Science and Engineering PAPER OPEN ACCESS CFD Studies on Triangular Micro-Vortex Generators in Flow Control To cite this article: V Yashodhar et al 2017 IOP Conf. Ser.:

More information

Experimental Investigation of End Plate Effects on the Vertical Axis Wind Turbine Airfoil Blade

Experimental Investigation of End Plate Effects on the Vertical Axis Wind Turbine Airfoil Blade Experimental Investigation of End Plate Effects on the Vertical Axis Wind Turbine Airfoil Blade Rikhi Ramkissoon 1, Krishpersad Manohar 2 Ph.D. Candidate, Department of Mechanical and Manufacturing Engineering,

More information

Lab 4: Pressure Gradients over a Wing

Lab 4: Pressure Gradients over a Wing 2009 Lab 4: Pressure Gradients over a Wing Innovative Scientific Solutions Inc. 2766 Indian Ripple Road Dayton, OH 45440 (937)-429-4980 Lab 4: Pressure Gradients over a Wing Introduction: Like the previous

More information

Investigation and Comparison of Airfoils

Investigation and Comparison of Airfoils AENG 360 Aerodynamics Investigation and Comparison of Airfoils Rocie Benavent Chelseyann Bipat Brandon Gilyard Julian Marcon New York Institute of Technology Fall 2013 2 Executive Summary Airfoil design

More information

DESIGN AND MANUFACTURING OF A MORPHING FLAP FOR WIND TURBINE BLADES

DESIGN AND MANUFACTURING OF A MORPHING FLAP FOR WIND TURBINE BLADES 6th ECCOMAS Conference on Smart Structures and Materials SMART2013 Politecnico di Torino, 24-26 June 2013 PB. Andersen, HAa. Madsen (Editors) www.smart2013.com DESIGN AND MANUFACTURING OF A MORPHING FLAP

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

EXPERIMENTAL ANALYSIS OF THE CONFLUENT BOUNDARY LAYER BETWEEN A FLAP AND A MAIN ELEMENT WITH SAW-TOOTHED TRAILING EDGE

EXPERIMENTAL ANALYSIS OF THE CONFLUENT BOUNDARY LAYER BETWEEN A FLAP AND A MAIN ELEMENT WITH SAW-TOOTHED TRAILING EDGE 24 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES EXPERIMENTAL ANALYSIS OF THE CONFLUENT BOUNDARY LAYER BETWEEN A FLAP AND A MAIN ELEMENT WITH SAW-TOOTHED TRAILING EDGE Lemes, Rodrigo Cristian,

More information

DOWNFORCE BALANCE. The Downforce Balance graph (shown at the left) illustrates which areas of the vehicle this product affects.

DOWNFORCE BALANCE. The Downforce Balance graph (shown at the left) illustrates which areas of the vehicle this product affects. OVERVIEW Spanning 67 (or 61) inches over its optimized 3D airfoil shape, the APR Performance GTC-300 Adjustable Wing supplies maximum downforce in sports and touring car applications. DOWNFORCE BALANCE

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

Aerofoil Profile Analysis and Design Optimisation

Aerofoil Profile Analysis and Design Optimisation Journal of Aerospace Engineering and Technology Volume 3, Issue 2, ISSN: 2231-038X Aerofoil Profile Analysis and Design Optimisation Kondapalli Siva Prasad*, Vommi Krishna, B.B. Ashok Kumar Department

More information

Numerical and Experimental Investigations of Lift and Drag Performances of NACA 0015 Wind Turbine Airfoil

Numerical and Experimental Investigations of Lift and Drag Performances of NACA 0015 Wind Turbine Airfoil International Journal of Materials, Mechanics and Manufacturing, Vol. 3, No., February 2 Numerical and Experimental Investigations of Lift and Drag Performances of NACA Wind Turbine Airfoil İzzet Şahin

More information

Effect of Leading Edge Radius and Blending Distance from Leading Edge on the Aerodynamic Performance of Small Wind Turbine Blade Airfoils

Effect of Leading Edge Radius and Blending Distance from Leading Edge on the Aerodynamic Performance of Small Wind Turbine Blade Airfoils International Journal of Energy and Power Engineering 2015; 4(5-1): 54-58 Published online September 6, 2015 (http://www.sciencepublishinggroup.com/j/ijepe) doi: 10.11648/j.ijepe.s.2015040501.19 ISSN:

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

Fin hydrodynamics of a windsurfer L. Sutherland & RA. Wilson Department of Ship Science, University of Southampton, Highfield, Southampton,

Fin hydrodynamics of a windsurfer L. Sutherland & RA. Wilson Department of Ship Science, University of Southampton, Highfield, Southampton, Fin hydrodynamics of a windsurfer L. Sutherland & RA. Wilson Department of Ship Science, University of Southampton, Highfield, Southampton, 1 Introduction Windsurfing is a relatively new technical sport

More information

DESIGN OF THE MODERN FAMILY OF HELICOPTER AIRFOILS

DESIGN OF THE MODERN FAMILY OF HELICOPTER AIRFOILS DESIGN OF THE MODERN FAMILY OF HELICOPTER AIRFOILS Wojciech KANIA, Wienczys!aw STALEWSKI, BogumHa ZWIERCHANOWSKA Institute of Aviation Summary The paper presents results of numerical design and experimental

More information

Design of the LRP airfoil series using 2D CFD

Design of the LRP airfoil series using 2D CFD Journal of Physics: Conference Series OPEN ACCESS Design of the LRP airfoil series using 2D CFD To cite this article: Frederik Zahle et al 2014 J. Phys.: Conf. Ser. 524 012020 View the article online for

More information

Design and Analysis of Vortex Generator and Dimple over an Airfoil Surface to Improve Aircraft Performance

Design and Analysis of Vortex Generator and Dimple over an Airfoil Surface to Improve Aircraft Performance ISSN: 2454-2377, Design and Analysis of Vortex Generator and Dimple over an Airfoil Surface to Improve Aircraft Performance Sonia Chalia 1*, Manish Kumar Bharti 2 1&2 Assistant professor, Department of

More information

Effect of High-Lift Devices on Aircraft Wing

Effect of High-Lift Devices on Aircraft Wing IOSR Journal of Engineering (IOSRJEN) ISSN (e): 2250-3021, ISSN (p): 2278-8719 PP 01-05 www.iosrjen.org Effect of High-Lift Devices on Aircraft Wing Gaurav B. Mungekar 1, Swapnil N. More 1, Samadhan V.

More information

Development process of a vertical axis wind turbine

Development process of a vertical axis wind turbine 7th World Summit for Small Wind (WSSW2016) / Technology Development Development process of a vertical axis wind turbine Daniel Lehser-Pfeffermann Wind energy lab, htw saar Germany Day 2 18.03.2016 7th

More information

Design and manufacturing of a morphing flap for wind turbine blades

Design and manufacturing of a morphing flap for wind turbine blades Downloaded from orbit.dtu.dk on: Nov 10, 2018 Design and manufacturing of a morphing flap for wind turbine blades Andersen, Peter Bjørn; Aagaard Madsen, Helge; Løgstrup Andersen, Tom; Schettler, Thomas

More information

EXPERIMENTAL INVESTIGATION OF WAKE SURVEY OVER A CYLINDER WITH DIFFERENT SURFACE PROFILES

EXPERIMENTAL INVESTIGATION OF WAKE SURVEY OVER A CYLINDER WITH DIFFERENT SURFACE PROFILES EXPERIMENTAL INVESTIGATION OF WAKE SURVEY OVER A CYLINDER WITH DIFFERENT SURFACE PROFILES Abdul Ahad Khan 1, Abhishek M. B 2, Tresa Harsha P George 3 1 Under Graduate student, Department of Aeronautical

More information

COMPUTER-AIDED DESIGN AND PERFORMANCE ANALYSIS OF HAWT BLADES

COMPUTER-AIDED DESIGN AND PERFORMANCE ANALYSIS OF HAWT BLADES 5 th International Advanced Technologies Symposium (IATS 09), May 13-15, 2009, Karabuk, Turkey COMPUTER-AIDED DESIGN AND PERFORMANCE ANALYSIS OF HAWT BLADES Emrah KULUNK a, * and Nadir YILMAZ b a, * New

More information

A Numerical Simulation Comparing the Efficiencies of Tubercle Versus Straight Leading Edge Airfoils for a Darrieus Vertical Axis Wind Turbine

A Numerical Simulation Comparing the Efficiencies of Tubercle Versus Straight Leading Edge Airfoils for a Darrieus Vertical Axis Wind Turbine A Numerical Simulation Comparing the Efficiencies of Tubercle Versus Straight Leading Edge Airfoils for a Darrieus Vertical Axis Wind Turbine By: Ross Neal Abstract: The efficiencies of sinusoidal and

More information

THE COLLEGE OF AERONAUTICS CRANFIELD

THE COLLEGE OF AERONAUTICS CRANFIELD THE COLLEGE OF AERONAUTICS CRANFIELD AERODYNAMIC CHARACTERISTICS OF A 40 SWEPT BACK WING OF ASPECT RATIO 4.5 by P. S. BARNA NOTE NO. 65 MAY, 1957 CRANFIELD A preliminary report on the aerodynamic characteristics

More information

IJSRD - International Journal for Scientific Research & Development Vol. 4, Issue 05, 2016 ISSN (online):

IJSRD - International Journal for Scientific Research & Development Vol. 4, Issue 05, 2016 ISSN (online): IJSRD - International Journal for Scientific Research & Development Vol. 4, Issue 0, 016 ISSN (online): 31-0613 Analysis of Transonic Flow over Airfoil using CFD for Gas Turbine Blades Kushal Gendcha 1

More information

Experimental and Theoretical Investigation for the Improvement of the Aerodynamic Characteristic of NACA 0012 airfoil

Experimental and Theoretical Investigation for the Improvement of the Aerodynamic Characteristic of NACA 0012 airfoil International Journal of Mining, Metallurgy & Mechanical Engineering (IJMMME) Volume 2, Issue 1 (214) ISSN 232 46 (Online) Experimental and Theoretical Investigation for the Improvement of the Aerodynamic

More information

Effect of Co-Flow Jet over an Airfoil: Numerical Approach

Effect of Co-Flow Jet over an Airfoil: Numerical Approach Contemporary Engineering Sciences, Vol. 7, 2014, no. 17, 845-851 HIKARI Ltd, www.m-hikari.com http://dx.doi.org/10.12988/ces.2014.4655 Effect of Co-Flow Jet over an Airfoil: Numerical Approach Md. Riajun

More information

Preliminary Analysis of Drag Reduction for The Boeing

Preliminary Analysis of Drag Reduction for The Boeing Preliminary Analysis of Drag Reduction for The Boeing 747-400 By: Chuck Dixon, Chief Scientist, Vortex Control Technologies LLC 07. 31. 2012 Potential for Airflow Separation That Can Be Reduced By Vortex

More information

CFD development for wind energy aerodynamics

CFD development for wind energy aerodynamics CFD development for wind energy aerodynamics Hamid Rahimi, Bastian Dose, Bernhard Stoevesandt Fraunhofer IWES, Germany IEA Task 40 Kick-off Meeting 12.11.2017 Tokyo Agenda BEM vs. CFD for wind turbine

More information

International Journal of Innovative Research in Science, Engineering and Technology Vol. 2, Issue 5, May 2013

International Journal of Innovative Research in Science, Engineering and Technology Vol. 2, Issue 5, May 2013 PERFORMANCE PREDICTION OF HORIZONTAL AXIS WIND TURBINE BLADE HardikPatel 1, SanatDamania 2 Master of Engineering Student, Department of Mechanical Engineering, Government Engineering College, Valsad, Gujarat,

More information

The Effect of Mounting Vortex Generators on the DTU 10MW Reference Wind Turbine Blade

The Effect of Mounting Vortex Generators on the DTU 10MW Reference Wind Turbine Blade Downloaded from orbit.dtu.dk on: Sep 14, 217 The Effect of Mounting Vortex Generators on the DTU 1MW Reference Wind Turbine Blade Skrzypinski, Witold Robert; Gaunaa, Mac; Bak, Christian Published in: Journal

More information

Numerical Investigation of Multi Airfoil Effect on Performance Increase of Wind Turbine

Numerical Investigation of Multi Airfoil Effect on Performance Increase of Wind Turbine International Journal of Engineering & Applied Sciences (IJEAS) International Journal of Engineering Applied Sciences (IJEAS) Vol.9, Issue 3 (2017) 75-86 Vol.x, Issue x(201x)x-xx http://dx.doi.org/10.24107/ijeas.332075

More information

INVESTIGATION OF PRESSURE CONTOURS AND VELOCITY VECTORS OF NACA 0015IN COMPARISON WITH OPTIMIZED NACA 0015 USING GURNEY FLAP

INVESTIGATION OF PRESSURE CONTOURS AND VELOCITY VECTORS OF NACA 0015IN COMPARISON WITH OPTIMIZED NACA 0015 USING GURNEY FLAP INVESTIGATION OF PRESSURE CONTOURS AND VELOCITY VECTORS OF NACA 0015IN COMPARISON WITH OPTIMIZED NACA 0015 USING GURNEY FLAP 1 ANANTH S SHARMA, 2 SUDHAKAR S, 3 SWATHIJAYAKUMAR, 4 B S ANIL KUMAR 1,2,3,4

More information

New aerodynamics rotor concepts. specifically for very large. offshore wind turbines

New aerodynamics rotor concepts. specifically for very large. offshore wind turbines New aerodynamics rotor concepts specifically for very large offshore wind turbines Deliverable 2.11 Edited by: Helge Aagaard Madsen, Leonardo Bergami, Flemming Rasmussen September 2013 Agreement no.: 308974

More information

Validation of the CQU-DTU-LN1 series of airfoils

Validation of the CQU-DTU-LN1 series of airfoils Journal of Physics: Conference Series OPEN ACCESS Validation of the CQU-DTU-LN1 series of airfoils To cite this article: W Z Shen et al 2014 J. Phys.: Conf. Ser. 555 012093 View the article online for

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

Aerodynamic Design, Fabrication and Testing of Wind Turbine Rotor Blades

Aerodynamic Design, Fabrication and Testing of Wind Turbine Rotor Blades Aerodynamic Design, Fabrication and Testing of Wind Turbine Rotor Blades T.Mahendrapandian Department of Mechanical Engineering P.G. Student, Regional Centre of Anna University, Tirunelveli, Tamilnadu,

More information

Principles of glider flight

Principles of glider flight Principles of glider flight [ Lecture 1: Lift, drag & glide performance ] Richard Lancaster Email: Richard@RJPLancaster.net Twitter: @RJPLancaster ASK-21 illustrations Copyright 1983 Alexander Schleicher

More information

Performance Analysis of the Flying Wing Airfoils

Performance Analysis of the Flying Wing Airfoils Performance Analysis of the Flying Wing Airfoils PRISACARIU Vasile Henri Coandă Air Force Academy, Brașov, Romania, aerosavelli73@yahoo.com Abstract Flying wings flight performances depend directly on

More information

Integrated airfoil and blade design method for large wind turbines

Integrated airfoil and blade design method for large wind turbines Downloaded from orbit.dtu.dk on: Oct 13, 2018 Integrated airfoil and blade design method for large wind turbines Zhu, Wei Jun; Shen, Wen Zhong Published in: Proceedings of the 2013 International Conference

More information

Aerofoil Design for Man Powered Aircraft

Aerofoil Design for Man Powered Aircraft Man Powered Aircraft Group Aerofoil Design for Man Powered Aircraft By F. X. Wortmann Universitat Stuttgart From the Second Man Powered Aircraft Group Symposium Man Powered Flight The Way Ahead 7 th February

More information

DEFINITIONS. Aerofoil

DEFINITIONS. Aerofoil Aerofoil DEFINITIONS An aerofoil is a device designed to produce more lift (or thrust) than drag when air flows over it. Angle of Attack This is the angle between the chord line of the aerofoil and the

More information

Increasing the power output of the Darrieus Vertical Axis Wind Turbine

Increasing the power output of the Darrieus Vertical Axis Wind Turbine 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36. Increasing the power output of the Darrieus Vertical Axis Wind Turbine R. Ramkissoon 1 and K. Manohar

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

2-D Computational Analysis of a Vertical Axis Wind Turbine Airfoil

2-D Computational Analysis of a Vertical Axis Wind Turbine Airfoil 2-D Computational Analysis of a Vertical Axis Wind Turbine Airfoil Akshay Basavaraj1 Student, Department of Aerospace Engineering, Amrita School of Engineering, Coimbatore 641 112, India1 Abstract: This

More information

Numerical and Experimental Investigation of the Possibility of Forming the Wake Flow of Large Ships by Using the Vortex Generators

Numerical and Experimental Investigation of the Possibility of Forming the Wake Flow of Large Ships by Using the Vortex Generators Second International Symposium on Marine Propulsors smp 11, Hamburg, Germany, June 2011 Numerical and Experimental Investigation of the Possibility of Forming the Wake Flow of Large Ships by Using the

More information

Air Craft Winglet Design and Performance: Cant Angle Effect

Air Craft Winglet Design and Performance: Cant Angle Effect Journal of Robotics and Mechanical Engineering Research Air Craft Winglet Design and Performance: Cant Angle Effect Eslam Said Abdelghany 1, Essam E Khalil 2*, Osama E Abdellatif 3 and Gamal elhariry 4

More information

Incompressible Flow over Airfoils

Incompressible Flow over Airfoils < 4.7 Classical Thin Airfoil Theory > The Symmetric Airfoil * Assumptions Incompressible Flow over Airfoils i) The camber line is one of the streamlines ii) Small maximum camber and thickness relative

More information

Flow Over Bodies: Drag and Lift

Flow Over Bodies: Drag and Lift Fluid Mechanics (0905241) Flow Over Bodies: Drag and Lift Dr.-Eng. Zayed dal-hamamre 1 Content Overview Drag and Lift Flow Past Objects Boundary Layers Laminar Boundary Layers Transitional and Turbulent

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

Effects of Leading-Edge Protection Tape on Wind Turbine Blade Performance

Effects of Leading-Edge Protection Tape on Wind Turbine Blade Performance Effects of Leading-Edge Protection Tape on Wind Turbine Blade Performance by Agrim Sareen, Chinmay A. Sapre and Michael S. Selig REPRINTED FROM WIND ENGINEERING VOLUME 36, NO. 5, 2012 MULTI-SCIENCE PUBLISHING

More information

Howard Torode. Member of General Aviation Group and Chairman BGA Technical Committee

Howard Torode. Member of General Aviation Group and Chairman BGA Technical Committee Efficient Light Aircraft Design Options from Gliding Howard Torode Member of General Aviation Group and Chairman BGA Technical Committee Presentation Aims Recognise the convergence of interest between

More information

NUMERICAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF NACA AIRFOIL WITH A GURNEY FLAP

NUMERICAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF NACA AIRFOIL WITH A GURNEY FLAP Int. J. Mech. Eng. & Rob. Res. 2012 MasoudJahanmorad Nouri et al., 2012 Research Paper ISSN 2278 0149 www.ijmerr.com Vol. 1, No. 3, October 2012 2012 IJMERR. All Rights Reserved NUMERICAL INVESTIGATION

More information