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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. (1996) Towards an Optimal Concept for Numerical Codes Simulating thrust Chamber processes in High Pressure Chemical Propulsion Systems. Acta Astronautica, Vol.38,, pp. 427-436.

Full text not available from this repository.

Abstract

Lampoldshausen 970219.

Item URL in elib:https://elib.dlr.de/25011/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=1996,
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:1996
Journal or Publication Title:Acta Astronautica
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:Vol.38,
Page Range:pp. 427-436
Status:Published
Keywords:Combustion Chamber Code, Physical Models, Numerical Models, Coupling, Flow Field Prediction-2
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 05:40

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