Isbn: 9786138934851 - cfd study for flow behavior of aerofoils (8 Ergebnisse)

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Taschenbuch. Zustand: Neu. CFD STUDY FOR FLOW BEHAVIOR OF AEROFOILS | Akhil Yuvaraj Manda (u. a.) | Taschenbuch | 56 S. | Englisch | 2020 | Scholars' Press | EAN 9786138934851 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu.…

Taschenbuch. Zustand: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The conception and examination for the aerofoil geometry have been executed in the current work to evaluate the behaviour of the flow in terms of the velocity and pressure lineation. The aerofoil geometries are opted to be of new aerofoil type of NACA 8412 series. The aerofoil geometry was analysed for a constant angle of attack along the total length. This evaluation was done for the angle of attack ranging from 0o to 20owith 5o interval for each model. The inlet velocity for the flow along the surface of the aerofoil geometry was taken varied from 7.5m/s to 10m/s with 0.5m/s interval for each model. The plot points for the geometries are generated using the Auto CAD for different angles. The further simulations and evaluations were executed using the Ansys Fluent software. On evaluating and considering the variable conditions, the optimum values are obtained for the aerofoil at 15o angle of inclination at an inlet velocity of 9m/s. The software generated results when compared to the regression data generated ascertained to be in a good correlation with each other 56 pp. Englisch.…

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Taschenbuch. Zustand: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The conception and examination for the aerofoil geometry have been executed in the current work to evaluate the behaviour of the flow in terms of the velocity and pressure lineation. The aerofoil geometries are opted to be of new aerofoil type of NACA 8412 series. The aerofoil geometry was analysed for a constant angle of attack along the total length. This evaluation was done for the angle of attack ranging from 0o to 20owith 5o interval for each model. The inlet velocity for the flow along the surface of the aerofoil geometry was taken varied from 7.5m/s to 10m/s with 0.5m/s interval for each model. The plot points for the geometries are generated using the Auto CAD for different angles. The further simulations and evaluations were executed using the Ansys Fluent software. On evaluating and considering the variable conditions, the optimum values are obtained for the aerofoil at 15o angle of inclination at an inlet velocity of 9m/s. The software generated results when compared to the regression data generated ascertained to be in a good correlation with each other.…

Taschenbuch. Zustand: Neu. This item is printed on demand - Print on Demand Titel. Neuware -The conception and examination for the aerofoil geometry have been executed in the current work to evaluate the behaviour of the flow in terms of the velocity and pressure lineation. The aerofoil geometries are opted to be of new aerofoil type of NACA 8412 series. The aerofoil geometry was analysed for a constant angle of attack along the total length. This evaluation was done for the angle of attack ranging from 0o to 20owith 5o interval for each model. The inlet velocity for the flow along the surface of the aerofoil geometry was taken varied from 7.5m/s to 10m/s with 0.5m/s interval for each model. The plot points for the geometries are generated using the Auto CAD for different angles. The further simulations and evaluations were executed using the Ansys Fluent software. On evaluating and considering the variable conditions, the optimum values are obtained for the aerofoil at 15o angle of inclination at an inlet velocity of 9m/s. The software generated results when compared to the regression data generated ascertained to be in a good correlation with each otherVDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 56 pp. Englisch.…