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X-38: A Testbed for the CEVCATS-N Code

Longo, J.M.A. and Lüdeke, H. and Brück, S. and Orlowski, M. and Rapuc, M. and Tribot, J.-P. and Stojanowski, M. (1999) X-38: A Testbed for the CEVCATS-N Code. Int. Symposium Atmospheric Reentry Vehicles and Systems, Arcachon (fr), 16.-18.03.1999.

Full text not available from this repository.

Abstract

The paper focuses on today possibility of using a Navier-Stokes code as design/verification tool for the hypersonic regime, on a real engineering environment. Within the frame of Dassault Aviation work for NASA X-38 demonstrator, DLR has performed more than two hundered CFD solutions, Euler and Navier-Stokes, demonstrating that the DLR computer code CEVCATS-N satisfies all criterion to be considered a reliable tool. That is, fulfilling concepts like accuracy, efficiency, flexibility and robustness for a wide spectrum of geometrical shapes and flow conditions.

Item URL in elib:https://elib.dlr.de/13525/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1999,
Title:X-38: A Testbed for the CEVCATS-N Code
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Longo, J.M.A.UNSPECIFIEDUNSPECIFIED
Lüdeke, H.UNSPECIFIEDUNSPECIFIED
Brück, S.UNSPECIFIEDUNSPECIFIED
Orlowski, M.UNSPECIFIEDUNSPECIFIED
Rapuc, M.UNSPECIFIEDUNSPECIFIED
Tribot, J.-P.UNSPECIFIEDUNSPECIFIED
Stojanowski, M.UNSPECIFIEDUNSPECIFIED
Date:1999
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:X-38, Crew Return Vehicle, CEVCATS, Hyperschall
Event Title:Int. Symposium Atmospheric Reentry Vehicles and Systems, Arcachon (fr), 16.-18.03.1999
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
Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik
Deposited By: Grant, Claudia
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 20:35

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