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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.

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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 Authors
Schley, C.-A.UNSPECIFIED
Hagemann, G.UNSPECIFIED
Krülle, G.UNSPECIFIED
Date:1997
Journal or Publication Title:Aerospace Science and Technology
Refereed publication:Yes
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 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 05:41

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