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Thermomechanical Analysis of Rocket Combustion Chamber

Kuhl, D. (1998) Thermomechanical Analysis of Rocket Combustion Chamber. In: Fourth World Congress on Computational Mechanics (Abstracts). Fourth World Congress on Computational Mechanics, Buenos Aires, Argentina, 29 June - 2 July, 1998.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/1421/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1999,
Title:Thermomechanical Analysis of Rocket Combustion Chamber
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Kuhl, D.UNSPECIFIEDUNSPECIFIED
Date:1998
Journal or Publication Title:Fourth World Congress on Computational Mechanics (Abstracts)
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmailEditor's ORCID iD
IACM, UNSPECIFIEDUNSPECIFIED
Status:Published
Keywords:Thermomechanical coupling; heat conduction; small strain plasticity; modeling of boundary conditions; rocket combustion chamber
Event Title:Fourth World Congress on Computational Mechanics, Buenos Aires, Argentina, 29 June - 2 July, 1998
Organizer:International Association for Computational Mechanics IACM
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 assignment
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Lohmiller, Monika
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:45

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