elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

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, 2016-07-25 - 2016-07-27, Salt Lake City, Utah, USA. doi: 10.2514/6.2016-4583.

[img] PDF
7MB

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 AuthorsAuthor's ORCID iDORCID Put Code
Thiede, Ray GordanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Riccius, JörgUNSPECIFIEDhttps://orcid.org/0000-0002-5935-874X139279978
Reese, S.RWTH AachenUNSPECIFIEDUNSPECIFIED
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:10.2514/6.2016-4583
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 Start Date:25 July 2016
Event End Date:27 July 2016
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Reusable Space Systems and Propulsion Technology
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:16 Nov 2016 07:48
Last Modified:24 Apr 2024 20:12

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.