9786139910304 - numerical investigation & performance comparison of aerofoil shapes di mehta, jaswinder singh (5 risultati)
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Da: moluna, Greven, Germaniamoluna
Contatta il venditoreVenditore con 5 stelleCondizione: Nuovo
EUR 34,25
EUR 48,99 spedizioneSpedito da Germania a U.S.A.Quantità: Più di 20 disponibili
Kartoniert / Broschiert. Condizione: New.
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Da: preigu, Osnabrück, Germaniapreigu
Contatta il venditoreVenditore con 5 stelleCondizione: Nuovo
EUR 36,35
EUR 70,00 spedizioneSpedito da Germania a U.S.A.Quantità: 5 disponibili
Taschenbuch. Condizione: 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.
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Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, GermaniaBuchWeltWeit Ludwig Meier e.K.
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EUR 39,90
EUR 23,00 spedizioneSpedito da Germania a U.S.A.Quantità: 2 disponibili
Taschenbuch. Condizione: 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 crit…erion 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.
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Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germaniabuchversandmimpf2000
Contatta il venditoreVenditore con 5 stelleCondizione: Nuovo
EUR 39,90
EUR 60,00 spedizioneSpedito da Germania a U.S.A.Quantità: 1 disponibili
Taschenbuch. Condizione: 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 criterio…n 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.
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Da: AHA-BUCH GmbH, Einbeck, GermaniaAHA-BUCH GmbH
Contatta il venditoreVenditore con 5 stelleCondizione: Nuovo
EUR 40,89
EUR 60,48 spedizioneSpedito da Germania a U.S.A.Quantità: 1 disponibili
Taschenbuch. Condizione: 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.
