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Modeling Experimental Flow Analysis by Ali Syed (5 results)
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Modeling and Experimental Flow Analysis around Airfoil
Published by LAP LAMBERT Academic Publishing Nov 2010, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Language: English
Seller: buchversandmimpf2000, Emtmannsberg, BAYE, Germany
Seller rating 5 out of 5 stars
US$ 59.56
Convert currencyUS$ 70.81 shipping from Germany to U.S.A.Quantity: 2 available
Add to basketTaschenbuch. Condition: 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.
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Modeling and Experimental Flow Analysis around Airfoil: Final Year Project (at GIKI Pakistan)
Published by LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Language: English
US$ 200.45
Convert currencyUS$ 33.79 shipping from United Kingdom to U.S.A.Quantity: 1 available
Add to basketPaperback. Condition: Like New. Like New. book.
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Modeling and Experimental Flow Analysis around Airfoil
Published by LAP LAMBERT Academic Publishing Nov 2010, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Language: English
Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germany
Seller rating 5 out of 5 stars
US$ 59.56
Convert currencyUS$ 27.14 shipping from Germany to U.S.A.Quantity: 2 available
Add to basketTaschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - 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. 76 pp. Englisch.
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Modeling and Experimental Flow Analysis around Airfoil
Published by LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Language: English
US$ 49.89
Convert currencyUS$ 57.81 shipping from Germany to U.S.A.Quantity: Over 20 available
Add to basketCondition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Ali Syed SarimSyed 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.
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Modeling and Experimental Flow Analysis around Airfoil : Final Year Project (at GIKI Pakistan)
Published by LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Language: English
US$ 59.56
Convert currencyUS$ 71.59 shipping from Germany to U.S.A.Quantity: 1 available
Add to basketTaschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - 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.
