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Simulation of Heat Transfer in Regeneratively Cooled Rocket Combustion Chambers

Woschnak, A. and Kuhl, D. (1998) Simulation of Heat Transfer in Regeneratively Cooled Rocket Combustion Chambers. In: Computational Fluid Dynamics '98, 1 und 2, pp. 1019-1024. John Wiley & Sons. ECCOMAS, Athens, Greece, 7-11 September 1998. ISBN 0-471-98579-1.

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Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1999,
Title:Simulation of Heat Transfer in Regeneratively Cooled Rocket Combustion Chambers
Authors:
AuthorsInstitution or Email of Authors
Woschnak, A.UNSPECIFIED
Kuhl, D.UNSPECIFIED
Date:1998
Journal or Publication Title:Computational Fluid Dynamics '98
Volume:1 und 2
Page Range:pp. 1019-1024
Editors:
EditorsEmail
Papailiou, K.D.UNSPECIFIED
Tsahalis, D.UNSPECIFIED
Periaux, J.UNSPECIFIED
Hirsch, C.UNSPECIFIED
Pandolfi, M.UNSPECIFIED
Publisher:John Wiley & Sons
Series Name:Proceedings of the Fourth European Computational Fluid Dynamics Conference
ISBN:0-471-98579-1
Status:Published
Keywords:Finite Element Method, Fluid Simulation, High Pressure, Cryogenic Rocket Combustor, Combustion Chambers Failure
Event Title:ECCOMAS, Athens, Greece, 7-11 September 1998
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 assignement
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Monika Lohmiller
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:41

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