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Towards an Optimal Concept for Numerical Codes Simulating Thrust Chamber Processes in High Pressure Chemical Propulsion Systems.

Schley, C.-A. and Hagemann, G. and Krülle, G. (1997) Towards an Optimal Concept for Numerical Codes Simulating Thrust Chamber Processes in High Pressure Chemical Propulsion Systems. Aerospace Science and Technology, Vol.1, Nr.3, pp. 203-213. Gauthier-Villars, Paris.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/25070/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=1997,
Title:Towards an Optimal Concept for Numerical Codes Simulating Thrust Chamber Processes in High Pressure Chemical Propulsion Systems.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schley, C.-A.UNSPECIFIEDUNSPECIFIED
Hagemann, G.UNSPECIFIEDUNSPECIFIED
Krülle, G.UNSPECIFIEDUNSPECIFIED
Date:1997
Journal or Publication Title:Aerospace Science and Technology
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:Vol.1, Nr.3
Page Range:pp. 203-213
Publisher:Gauthier-Villars, Paris
Status:Published
Keywords:Computational fluid dynamics, Numerical modelling, Physical modelling, Rocket engines,
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 05:41

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