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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.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/25140/
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 AuthorsAuthors ORCID iD
Koschel, W.UNSPECIFIEDUNSPECIFIED
Link, T.RWTH AachenUNSPECIFIED
Fox, U.RWTH AachenUNSPECIFIED
Date:1998
Journal or Publication Title:AIAA 8th Intern. Space Planes and Hypersonic Systems and Technologies Conference, April 27-30, 1998, Norfolk, VA
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
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 assignment
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:43

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