Modeling and Experimental Flow Analysis around Airfoil

Syed Sarim Ali

ISBN 10: 3843359784 / ISBN 13: 9783843359788

Published by LAP LAMBERT Academic Publishing Nov 2010, 2010

About this Item

Neuware -In this project, Modeling and Experimental Analysis of Flow over Different Airfoils, an attempt is made to find different aerodynamic parameters of airfoils. Analytical Solution of pressure Distribution, Lift and Drag Coefficients shall be obtained by solving the model in CFX. Analytical results will then be validated by using the wind tunnel instrumentation system. The actual values of lift and drag attained from wind tunnel will be compared with the results from analytical solution. Once the analytical model is verified, model will further tested by changing the pre-defined parameters. At the end graph will be plotted for different values of lift and drag against the angle of attack of the airfoil.Books on Demand GmbH, Überseering 33, 22297 Hamburg 76 pp. Englisch.

Seller Inventory # 9783843359788

Bibliographic Details

• Title: Modeling and Experimental Flow Analysis around Airfoil
• Publisher: LAP LAMBERT Academic Publishing Nov 2010
• Publication Date: 2010
• Language: English
• ISBN 10: 3843359784
• ISBN 13: 9783843359788
• Binding: Taschenbuch
• Condition: Neu
• Dimensions: 220W x 150H x 5D millimeters 220 millimeters width by 150 millimeters height by 5 millimeters depth
• Weight: 131 grams

About this title

Synopsis

In this project, Modeling and Experimental Analysis of Flow over Different Airfoils, an attempt is made to find different aerodynamic parameters of airfoils. Analytical Solution of pressure Distribution, Lift and Drag Coefficients shall be obtained by solving the model in CFX. Analytical results will then be validated by using the wind tunnel instrumentation system. The actual values of lift and drag attained from wind tunnel will be compared with the results from analytical solution. Once the analytical model is verified, model will further tested by changing the pre-defined parameters. At the end graph will be plotted for different values of lift and drag against the angle of attack of the airfoil.

About the Author

Syed Sarim Ali is a graduate of Ghulam Ishaq Khan Institute, one of the highest ranked engineering institution in Pakistan. He has also been involved in various engineering competition mainly focusing on aircraft design. He has also represented Pakistan in 47th International Mathematics Olympiad and 18th Asian Pacific Mathematics Olympiad