Synopsis
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.
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About the Author
Mr. J. Chandra Shekar completed his Masters Degree in CAD/CAM.Have professional experience of 3.10 years as Design Engineer.Proficient in Design Tools like CATIA-V5R19 and AutoCAD-2009.Proficient in Meshing Tool like ICEM-CFD 10/13.
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Numerical Analysis of Boundary Layer Flow Over 3D Aerofoil Section
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LAP LAMBERT Academic Publishing Okt 2014, 2014
ISBN 10: 3659618896
ISBN 13: 9783659618895
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Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -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. 148 pp. Englisch. Seller Inventory # 9783659618895
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Numerical Analysis of Boundary Layer Flow Over 3D Aerofoil Section
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LAP LAMBERT Academic Publishing, 2014
ISBN 10: 3659618896
ISBN 13: 9783659618895
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Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Chandra Shekar J.Mr. J. Chandra Shekar completed his Masters Degree in CAD/CAM.Have professional experience of 3.10 years as Design Engineer.Proficient in Design Tools like CATIA-V5R19 and AutoCAD-2009.Proficient in Meshing Tool like. Seller Inventory # 5168779
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Numerical Analysis of Boundary Layer Flow Over 3D Aerofoil Section
Published by
LAP LAMBERT Academic Publishing Okt 2014, 2014
ISBN 10: 3659618896
ISBN 13: 9783659618895
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Taschenbuch
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Taschenbuch. Condition: Neu. This item is printed on demand - Print on Demand Titel. Neuware -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.Books on Demand GmbH, Überseering 33, 22297 Hamburg 148 pp. Englisch. Seller Inventory # 9783659618895
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Numerical Analysis of Boundary Layer Flow Over 3D Aerofoil Section | CFD Analysis
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LAP LAMBERT Academic Publishing, 2014
ISBN 10: 3659618896
ISBN 13: 9783659618895
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Taschenbuch. Condition: Neu. Numerical Analysis of Boundary Layer Flow Over 3D Aerofoil Section | CFD Analysis | J. Chandra Shekar (u. a.) | Taschenbuch | 148 S. | Englisch | 2014 | LAP LAMBERT Academic Publishing | EAN 9783659618895 | Verantwortliche Person für die EU: BoD - Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu. Seller Inventory # 105002763
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Numerical Analysis of Boundary Layer Flow Over 3D Aerofoil Section : CFD Analysis
Published by
LAP LAMBERT Academic Publishing, 2014
ISBN 10: 3659618896
ISBN 13: 9783659618895
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Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - 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. Seller Inventory # 9783659618895
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Numerical Analysis of Boundary Layer Flow Over 3D Aerofoil Section: CFD Analysis
Published by
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ISBN 10: 3659618896
ISBN 13: 9783659618895
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