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Numerical Analysis of Boundary Layer Flow Over 3D Aerofoil Section

 

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  • Product Description
 

In the present study, the numerical study is carried out for boundary layer flow over 3D aerofoil section and the aerodynamic performance of NACA aerofoil are analyzed by studying the lift and drag coefficient of the aerofoil.The results obtained in the case of boundary layer flow over the 3D aerofoil section are compared with the experimental data as available in the literature. The experimental data for NACA 64-009 from wind tunnel is validated with simulations results computed in FLUENT. The aerofoil is cambered and measured to be around 1mt. The simulations for boundary layer flow for NACA 64-009 is performed at various angles of attacks. In addition, the lift coefficient, drag coefficient, pressure contour and velocity contour are computed.

Product Specifications
SKU :COC54772
AuthorJ. Chandra Shekar and Aditya Kolakoti
LanguageEnglish
BindingPaperback
Number of Pages148
Publishing Year2014-10-31T00:00:00.000
ISBN9783659618895
Edition1 st
Book TypeIndustry & industrial studies
Country of ManufactureIndia
Product BrandLAP LAMBERT Academic Publishing
Product Packaging InfoBox
In The Box1 Piece
Product First Available On ClickOnCare.com2015-06-08 00:00:00
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