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Vortex Flow on a Hypersonic Spaceplane-type Configuration

Herrmann, U. (1993) Vortex Flow on a Hypersonic Spaceplane-type Configuration. Euromech 312, Turbulence and Vortices in Hypersonic Flows Goettingen, 5.10.1993-7.10.1993.

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Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1993,
Title:Vortex Flow on a Hypersonic Spaceplane-type Configuration
Authors:
AuthorsInstitution or Email of Authors
Herrmann, U.UNSPECIFIED
Date:1993
Status:Published
Keywords:Hypersonic inviscid flow, conical Euler calculation, mesh refinement, shock induced seperation from smooth surfaces, flux vector splitting upwind scheme, comparison with measured data
Event Title:Euromech 312, Turbulence and Vortices in Hypersonic Flows Goettingen, 5.10.1993-7.10.1993
HGF - Research field:UNSPECIFIED
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:UNSPECIFIED
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Grundlagen Raumtransport - Anlagen und Messtechnik (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:05

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