Publicado por LAP LAMBERT Academic Publishing Nov 2010, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Idioma: Inglés
Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemania
EUR 49,00
Cantidad disponible: 2 disponibles
Añadir al carritoTaschenbuch. Condición: 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.
Publicado por LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Idioma: Inglés
Librería: preigu, Osnabrück, Alemania
EUR 43,10
Cantidad disponible: 5 disponibles
Añadir al carritoTaschenbuch. Condición: Neu. Modeling and Experimental Flow Analysis around Airfoil | Final Year Project (at GIKI Pakistan) | Syed Sarim Ali (u. a.) | Taschenbuch | 76 S. | Englisch | 2010 | LAP LAMBERT Academic Publishing | EAN 9783843359788 | Verantwortliche Person für die EU: BoD - Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu.
Publicado por LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Idioma: Inglés
Librería: Mispah books, Redhill, SURRE, Reino Unido
EUR 168,66
Cantidad disponible: 1 disponibles
Añadir al carritoPaperback. Condición: Like New. Like New. Ships from Multiple Locations. book.
Publicado por LAP LAMBERT Academic Publishing Nov 2010, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Idioma: Inglés
Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Alemania
EUR 49,00
Cantidad disponible: 2 disponibles
Añadir al carritoTaschenbuch. Condición: 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.
Publicado por LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Idioma: Inglés
Librería: moluna, Greven, Alemania
EUR 41,05
Cantidad disponible: Más de 20 disponibles
Añadir al carritoCondición: 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.
Publicado por LAP LAMBERT Academic Publishing, 2010
ISBN 10: 3843359784 ISBN 13: 9783843359788
Idioma: Inglés
Librería: AHA-BUCH GmbH, Einbeck, Alemania
EUR 49,00
Cantidad disponible: 1 disponibles
Añadir al carritoTaschenbuch. Condición: 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.