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Computation of Hypersonic Propulsion System Expansion Flows Considering Hydrogen/Air High Temperature Effects

Koschel, W. and Link, T. and Fox, U. (1998) Computation of Hypersonic Propulsion System Expansion Flows Considering Hydrogen/Air High Temperature Effects. In: AIAA 8th Intern. Space Planes and Hypersonic Systems and Technologies Conference, April 27-30, 1998, Norfolk, VA.

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Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1998,
Title:Computation of Hypersonic Propulsion System Expansion Flows Considering Hydrogen/Air High Temperature Effects
Authors:
AuthorsInstitution or Email of Authors
Koschel, W.UNSPECIFIED
Link, T.RWTH Aachen
Fox, U.RWTH Aachen
Date:1998
Journal or Publication Title:AIAA 8th Intern. Space Planes and Hypersonic Systems and Technologies Conference, April 27-30, 1998, Norfolk, VA
Series Name:AIAA 98-1601
Status:Published
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):E -- no assignement
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: elib DLR-Beauftragter
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:43

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