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In den WarenkorbZustand: New. KlappentextrnrnThe objective of this research is to develop a prediction code for the Air Force Research Laboratory Propulsion Directorate that can accurately determine the gross thrust coefficient for a user defined non-axisymmetric two-dimensi.
Sprache: Englisch
Verlag: Creative Media Partners, LLC, 2012
ISBN 10: 1249450039 ISBN 13: 9781249450030
Anbieter: PBShop.store US, Wood Dale, IL, USA
PAP. Zustand: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.
Sprache: Englisch
Verlag: Creative Media Partners, LLC Sep 2012, 2012
ISBN 10: 1249450039 ISBN 13: 9781249450030
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
Taschenbuch. Zustand: Neu. Neuware - The objective of this research is to develop a prediction code for the Air Force Research Laboratory Propulsion Directorate that can accurately determine the gross thrust coefficient for a user defined non-axisymmetric two-dimensional converging diverging nozzle. The code includes the effects of friction, angularity, and expansion losses on nozzle efficiency. To demonstrate the prediction method, the generated computational results were compared to experimental data, as well as computational results from other existing nozzle performance codes, for a number of different nozzle geometries. The nozzle internal performance prediction code showed excellent agreement with experimental data in predicting the gross thrust performance for all nozzle geometries considered. It was shown, however, that when the experimental data showed evidence of flow separation, a flow phenomenon this code is unable to predict, the code results underpredicted the experimental by up to 10%.
Sprache: Englisch
Verlag: Creative Media Partners, LLC, 2012
ISBN 10: 1249450039 ISBN 13: 9781249450030
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In den WarenkorbZustand: New. Print on Demand pp. 122.
Zustand: New. Print on Demand pp. 122.
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