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Flow Simulation past the HALIS Configuration at Cold Wind Tunnel Conditions

Longo, J.M.A. and Nickel, H. (1994) Flow Simulation past the HALIS Configuration at Cold Wind Tunnel Conditions. In: DLR Contribution to the Fourth European High Velocity Database Workshop (ESTEC, Noordwijk, November 1994), pp. 81-92. 4th European High Velocity Database Workshop, Noordwijk (nl), 24.-25.11.1994. ISBN ISSN 1434-8454.

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Abstract

In the present study, computed results for a modified US Space Shuttle Orbiter are presented for the test case No. 8 defined for the Fourth European High-Velocity Database Workshop. This modified orbiter configuration was also tested in the USA numerically [WGG93] and experimentally [BPW94]. The conditions for the flow simulation correspond to the experiments carried out by Dassault Aviation [GSB94] at ONERA S4 Modane: Mach number 9.8, total temperature 1100K, Reynolds number 0.61 x 10 millions, incidence 40°, body-flap deflection 15°, surface temperature 300K. In the following sections a description of the computational grid used is presented, followed by a summary of the characteristics of the computer code. Then, the numerical accuracy of the solution is discussed by means of convergence studies and correlation with the available experimental data. Finally, some remarks are formulated.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2005,
Title:Flow Simulation past the HALIS Configuration at Cold Wind Tunnel Conditions
Authors:
AuthorsInstitution or Email of Authors
Longo, J.M.A.UNSPECIFIED
Nickel, H.UNSPECIFIED
Date:1994
Journal or Publication Title:DLR Contribution to the Fourth European High Velocity Database Workshop (ESTEC, Noordwijk, November 1994)
Page Range:pp. 81-92
Editors:
EditorsEmail
Kordulla, W.UNSPECIFIED
Brück, S.UNSPECIFIED
Series Name:DLR-FB 97-34
ISBN:ISSN 1434-8454
Status:Published
Keywords:Hypersonic, Perfect Gas, Re-entry, Wing, CFD
Event Title:4th European High Velocity Database Workshop, Noordwijk (nl), 24.-25.11.1994
Organizer:ESTEC
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
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: Claudia Grant
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 20:21

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