Ali syed sarim (5 resultados)

- Tapa blanda
Librería: Mispah books, Redhill, SURRE, Reino UnidoMispah books
Contactar con el vendedorVendedor de 4 estrellasCondición: Usado - Como Nuevo
EUR 175,23
Envío por EUR 29,54Se envía de Reino Unido a Estados Unidos de AmericaCantidad disponible: 1 disponible
Paperback. Condición: Like New. LIKE NEW. SHIPS FROM MULTIPLE LOCATIONS. book.

- Tapa blanda
- Impresión bajo demanda
Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, AlemaniaBuchWeltWeit Ludwig Meier e.K.
Contactar con el vendedorVendedor de 5 estrellasCondición: Nuevo
EUR 49,00
Envío por EUR 23,00Se envía de Alemania a Estados Unidos de AmericaCantidad disponible: 2 disponibles
Taschenbuch. 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.…

- Tapa blanda
- Impresión bajo demanda
Librería: AHA-BUCH GmbH, Einbeck, AlemaniaAHA-BUCH GmbH
Contactar con el vendedorVendedor de 5 estrellasCondición: Nuevo
EUR 54,70
Envío por EUR 35,00Se envía de Alemania a Estados Unidos de AmericaCantidad disponible: 1 disponible
Taschenbuch. 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. …

- Tapa blanda
- Impresión bajo demanda
Librería: moluna, Greven, Alemaniamoluna
Contactar con el vendedorVendedor de 5 estrellasCondición: Nuevo
EUR 41,05
Envío por EUR 48,99Se envía de Alemania a Estados Unidos de AmericaCantidad disponible: Más de 20 disponibles
Condición: 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.…

- Tapa blanda
- Impresión bajo demanda
Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemaniabuchversandmimpf2000
Contactar con el vendedorVendedor de 5 estrellasCondición: Nuevo
EUR 49,00
Envío por EUR 60,00Se envía de Alemania a Estados Unidos de AmericaCantidad disponible: 1 disponible
Taschenbuch. Condición: Neu. This item is printed on demand - Print on Demand Titel. 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.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 76 pp. Englisch. …