Editore: LAP LAMBERT Academic Publishing Nov 2010, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Lingua: Inglese
Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germania
EUR 49,00
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Aggiungi al carrelloTaschenbuch. Condizione: 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.
Editore: LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Lingua: Inglese
Da: Mispah books, Redhill, SURRE, Regno Unito
EUR 169,60
Convertire valutaQuantità: 1 disponibili
Aggiungi al carrelloPaperback. Condizione: Like New. Like New. book.
Editore: LAP LAMBERT Academic Publishing Nov 2010, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Lingua: Inglese
Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germania
EUR 49,00
Convertire valutaQuantità: 2 disponibili
Aggiungi al carrelloTaschenbuch. Condizione: 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.
Editore: LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Lingua: Inglese
Da: moluna, Greven, Germania
EUR 41,05
Convertire valutaQuantità: Più di 20 disponibili
Aggiungi al carrelloCondizione: 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.
Editore: LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Lingua: Inglese
Da: AHA-BUCH GmbH, Einbeck, Germania
EUR 49,00
Convertire valutaQuantità: 1 disponibili
Aggiungi al carrelloTaschenbuch. Condizione: 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.