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Modeling and Experimental Flow Analysis Around Airfoil: Final Year Project (at GIKI Pakistan) - Softcover
Inhaltsangabe
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.
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Über die Autorin bzw. den Autor
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
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Modeling and Experimental Flow Analysis around Airfoil
Verlag:
LAP LAMBERT Academic Publishing Nov 2010, 2010
ISBN 10: 3843359784
ISBN 13: 9783843359788
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Taschenbuch
Anbieter: buchversandmimpf2000, Emtmannsberg, BAYE, Deutschland
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Taschenbuch. Zustand: Neu. 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. Artikel-Nr. 9783843359788
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