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Modeling and Experimental Flow Analysis around Airfoil: Final Year Project (at GIKI Pakistan)

-15% su kodu: ENG15
59,95 
Įprasta kaina: 70,53 
-15% su kodu: ENG15
Kupono kodas: ENG15
Akcija baigiasi: 2025-03-03
-15% su kodu: ENG15
59,95 
Įprasta kaina: 70,53 
-15% su kodu: ENG15
Kupono kodas: ENG15
Akcija baigiasi: 2025-03-03
-15% su kodu: ENG15
2025-02-28 70.5300 InStock
Nemokamas pristatymas į paštomatus per 11-15 darbo dienų užsakymams nuo 20,00 

Knygos aprašymas

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.

Informacija

Autorius: Syed Sarim Ali, Mohammad Talha, Hasan Fawad Junejo,
Leidėjas: LAP LAMBERT Academic Publishing
Išleidimo metai: 2010
Knygos puslapių skaičius: 76
ISBN-10: 3843359784
ISBN-13: 9783843359788
Formatas: 220 x 150 x 5 mm. Knyga minkštu viršeliu
Kalba: Anglų

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