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.

Full text not available from this repository.

Document Type:

Conference or Workshop Item (Paper)

Additional Information:

LIDO-Berichtsjahr=1999,

Title:

Simulation of Heat Transfer in Regeneratively Cooled Rocket Combustion Chambers

Authors:

Authors	Institution or Email of Authors
Woschnak, A.
Kuhl, D.

Date:

1998

Journal or Publication Title:

Computational Fluid Dynamics '98

Volume:

1 und 2

Page Range:

pp. 1019-1024

Editors:

Editors	Email
Papailiou, K.D.
Tsahalis, D.
Periaux, J.
Hirsch, C.
Pandolfi, M.

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

HGF - Program:

Space

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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