Dynamics of inviscid compressible flow is governed by the Euler equations. Unsteady Euler equations are always hyperbolic. Upwind methods take into account the wave-like behavior of the hyperbolic systems and they are found to be more successful in numerical computation compared with central difference methods accompanied by artificial viscosity. Computation of flows governed by compressible Euler equations around such configurations like wing, aircraft, missile and launch vehicles are some situations where upwind schemes are extensively used. These schemes are not uniformly good for all situations. The relative merits and demerits of different upwind schemes by applying them for different flow situations like shock tube problem and 1-D quasi nozzle.
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Harinath Reddy Nakkala arbeitet derzeit als Assistenzprofessor in der Abteilung für Maschinenbau am Y.S.R. Engineering College der Yogi Vemana University, Proddatur, Andhra Pradesh, Indien. Vor seiner Lehrtätigkeit arbeitete er 8,5 Jahre lang bei Cyient, Hyderabad, Indien, im Bereich Luft- und Raumfahrt.
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Zustand: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Dynamics of inviscid compressible flow is governed by the Euler equations. Unsteady Euler equations are always hyperbolic. Upwind methods take into account the wave-like behavior of the hyperbolic systems and they are found to be more successful in numerica. Bestandsnummer des Verkäufers 1660040937
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Taschenbuch. Zustand: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Dynamics of inviscid compressible flow is governed by the Euler equations. Unsteady Euler equations are always hyperbolic. Upwind methods take into account the wave-like behavior of the hyperbolic systems and they are found to be more successful in numerical computation compared with central difference methods accompanied by artificial viscosity. Computation of flows governed by compressible Euler equations around such configurations like wing, aircraft, missile and launch vehicles are some situations where upwind schemes are extensively used. These schemes are not uniformly good for all situations. The relative merits and demerits of different upwind schemes by applying them for different flow situations like shock tube problem and 1-D quasi nozzle.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 60 pp. Englisch. Bestandsnummer des Verkäufers 9786207471454
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Taschenbuch. Zustand: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Dynamics of inviscid compressible flow is governed by the Euler equations. Unsteady Euler equations are always hyperbolic. Upwind methods take into account the wave-like behavior of the hyperbolic systems and they are found to be more successful in numerical computation compared with central difference methods accompanied by artificial viscosity. Computation of flows governed by compressible Euler equations around such configurations like wing, aircraft, missile and launch vehicles are some situations where upwind schemes are extensively used. These schemes are not uniformly good for all situations. The relative merits and demerits of different upwind schemes by applying them for different flow situations like shock tube problem and 1-D quasi nozzle. Bestandsnummer des Verkäufers 9786207471454
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Taschenbuch. Zustand: Neu. Computation of High-Speed Inviscid Compressible Flow by Upwind Schemes | Harinath Reddy Nakkala | Taschenbuch | Englisch | 2024 | LAP LAMBERT Academic Publishing | EAN 9786207471454 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. Bestandsnummer des Verkäufers 129211782
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