The book is founded on investigating the performance of different aerofoil shapes at varying angles of attack by conducting numerical investigation. The performance of the aerofoil shapes has been evaluated on the basis of the criterion of lift force generation as the aerofoils are designed in such a way that they generate maximum amount of lift. Different plots such as velocity contours and coefficient of lift and coefficient of drag versus different angles of attack have also been plotted for assessing the performance of different aerofoil shapes.
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Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germany
Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The book is founded on investigating the performance of different aerofoil shapes at varying angles of attack by conducting numerical investigation. The performance of the aerofoil shapes has been evaluated on the basis of the criterion of lift force generation as the aerofoils are designed in such a way that they generate maximum amount of lift. Different plots such as velocity contours and coefficient of lift and coefficient of drag versus different angles of attack have also been plotted for assessing the performance of different aerofoil shapes. 52 pp. Englisch. Seller Inventory # 9786139910304
Seller: moluna, Greven, Germany
Kartoniert / Broschiert. Condition: New. Seller Inventory # 498828619
Quantity: Over 20 available
Seller: buchversandmimpf2000, Emtmannsberg, BAYE, Germany
Taschenbuch. Condition: Neu. This item is printed on demand - Print on Demand Titel. Neuware -The book is founded on investigating the performance of different aerofoil shapes at varying angles of attack by conducting numerical investigation. The performance of the aerofoil shapes has been evaluated on the basis of the criterion of lift force generation as the aerofoils are designed in such a way that they generate maximum amount of lift. Different plots such as velocity contours and coefficient of lift and coefficient of drag versus different angles of attack have also been plotted for assessing the performance of different aerofoil shapes.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 52 pp. Englisch. Seller Inventory # 9786139910304
Seller: AHA-BUCH GmbH, Einbeck, Germany
Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The book is founded on investigating the performance of different aerofoil shapes at varying angles of attack by conducting numerical investigation. The performance of the aerofoil shapes has been evaluated on the basis of the criterion of lift force generation as the aerofoils are designed in such a way that they generate maximum amount of lift. Different plots such as velocity contours and coefficient of lift and coefficient of drag versus different angles of attack have also been plotted for assessing the performance of different aerofoil shapes. Seller Inventory # 9786139910304
Seller: preigu, Osnabrück, Germany
Taschenbuch. Condition: Neu. Numerical Investigation & Performance Comparison of Aerofoil Shapes | Jaswinder Singh Mehta | Taschenbuch | Englisch | 2021 | LAP LAMBERT Academic Publishing | EAN 9786139910304 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. Seller Inventory # 120488966