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Comparison of High Pressure h2/O2 Rocket Model-Engine 2D-Reference-Simulation Results

Schley, C.-A. and Golovitchev, V. and Hagemann, G. (1995) Comparison of High Pressure h2/O2 Rocket Model-Engine 2D-Reference-Simulation Results. In: AIAA. 31st AIAA Joint Propulsion Conference and Exhibit July 10-12, 1995 / San Diego, CA.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/24898/
Document Type:Conference or Workshop Item (Paper)
Additional Information: institution=AIAA, LIDO-Berichtsjahr=1995, pages=11,
Title:Comparison of High Pressure h2/O2 Rocket Model-Engine 2D-Reference-Simulation Results
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schley, C.-A.UNSPECIFIEDUNSPECIFIED
Golovitchev, V.UNSPECIFIEDUNSPECIFIED
Hagemann, G.UNSPECIFIEDUNSPECIFIED
Date:1995
Journal or Publication Title:AIAA
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Series Name:AIAA-95-2429
Status:Published
Keywords:Rocket Combustion Chamber, Numerical Simulation, 2D Geometry, Coaxial Injection, Physical Sub Models
Event Title:31st AIAA Joint Propulsion Conference and Exhibit July 10-12, 1995 / San Diego, CA
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):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 05:37

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