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Comparison of Damage Parameter Based Finite Element Fatigue Life Analysis Results to Combustion Chamber Type TMF Panel Test Results

Thiede, Ray Gordan and Zametaev, E. B. and Riccius, Jörg and Fassin, M. and Reese, S. (2015) Comparison of Damage Parameter Based Finite Element Fatigue Life Analysis Results to Combustion Chamber Type TMF Panel Test Results. In: 51st AIAA/SAE/ASEE Joint Propulsion Conference. 51st AIAA/SAE/ASEE Joint Propulsion Conference, 27.-29. Jul. 2015, Orlando, USA.

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Item URL in elib:https://elib.dlr.de/99733/
Document Type:Conference or Workshop Item (Speech)
Title:Comparison of Damage Parameter Based Finite Element Fatigue Life Analysis Results to Combustion Chamber Type TMF Panel Test Results
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Thiede, Ray GordanGordan.Thiede (at) dlr.deUNSPECIFIED
Zametaev, E. B.Evgeny.Zametaev (at) dlr.deUNSPECIFIED
Riccius, JörgJoerg.Riccius (at) dlr.deUNSPECIFIED
Fassin, M.RWTH AachenUNSPECIFIED
Reese, S.RWTH AachenUNSPECIFIED
Date:2015
Journal or Publication Title:51st AIAA/SAE/ASEE Joint Propulsion Conference
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:TMF panel, rocket combustion chamber, low cycle fatigue lifetime estimation, FEM
Event Title:51st AIAA/SAE/ASEE Joint Propulsion Conference
Event Location:Orlando, USA
Event Type:international Conference
Event Dates:27.-29. Jul. 2015
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Antriebsystemtechnik - Schubkammertechnologie
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:23 Nov 2015 13:44
Last Modified:31 Jul 2019 19:56

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