high speed computation (8 résultats)

Hardcover. Etat : Très bon. Ancien livre de bibliothèque. Légères traces d'usure sur la couverture. Couverture différente. Edition 1984. Ammareal reverse jusqu'à 15% du prix net de cet article à des organisations caritatives. ENGLISH DESCRIPTION Book Condition: Used, Very good. Former library book. Slight signs of wear on the cover. Different cover. Edition 1984. Ammareal gives back up to 15% of this item's net price to charity organizations.

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hardcover. Etat : Sehr gut. 441 p. In very good condition. ISBN: 9783540128854 Sprache: Englisch Gewicht in Gramm: 882.

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Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware 60 pp. Englisch.

Etat : 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.

Taschenbuch. Etat : 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.

Taschenbuch. Etat : 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.