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

Thiede, Ray Gordan and Riccius, Jörg and Reese, S. (2016) Validation of Damage Parameter Based Finite Element Fatigue Life Analysis Results to Combustion Chamber Type TMF Panel Test Results. In: 52nd AIAA/SAE/ASEE Joint Propulsion Conference. 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 25.-27. Juli 2016, Salt Lake City, Utah, USA. DOI: 10.2514/6.2016-5094

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Item URL in elib:https://elib.dlr.de/107782/
Document Type:Conference or Workshop Item (Speech)
Title:Validation 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
Riccius, JörgJoerg.Riccius (at) dlr.deUNSPECIFIED
Reese, S.RWTH AachenUNSPECIFIED
Date:27 July 2016
Journal or Publication Title:52nd 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
DOI :10.2514/6.2016-5094
Status:Published
Keywords:viscoplasticity, continuum damage mechanics, FEM modelling, life prediction, doghouse effect, crack-closure effect
Event Title:52nd AIAA/SAE/ASEE Joint Propulsion Conference
Event Location:Salt Lake City, Utah, USA
Event Type:international Conference
Event Dates:25.-27. Juli 2016
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 - Wiederverwendbare Raumfahrtsysteme und Antriebstechnologie
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:16 Nov 2016 07:48
Last Modified:31 Jul 2019 20:04

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