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Comparison of Finite Element analysis and experimental results of a combustion chamber type TMF panel test

Riccius, Jörg and Bouajila, W. and Zametaev, E. (2013) Comparison of Finite Element analysis and experimental results of a combustion chamber type TMF panel test. In: Proceedings. 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2013-07-14 - 2013-07-17, San Jose, CA, USA. doi: 10.2514/6.2013-3846.

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The inner liner of a regeneratively cooled wall of a main stage rocket combustion chamber is extremely loaded by the high temperature of the hot gas and the pressure difference between the coolant and the hot gas. A cyclic operation of such a chamber usually causes a LFC failure of the wall structure after a very low number of cycles. For the tests presented in this paper, cyclic laser heating is (as replacement for the hot gas) applied to an actively cooled small section of the hot gas wall of the real engine - the so called TMF panel. Optical measurements during such TMF panel tests provide essential validation data for CFD, thermal, structural and fatigue life analyses: The 2d measurement of the thermal field of the heat loaded structure provides - together with the measurement of the temperature, pressure and mass flow rate of the coolant of the TMF panel - data for the combined validation of the CFD analysis of the coolant flow and the thermal analysis of the wall structure. The measurement of the deformation of the thermally loaded structure provides - together with the already determined temperature distribution and the above mentioned pressure measurements of the cooling channels - data for the validation of the structural analysis of the thermally loaded structure. Counting the number of laser loading cycles (laser on-off) until the TMF panel fails (by cracks appearing on the laser loaded side of the cooling channels) provides data for the validation of (either post processing or damage parameter based) fatigue life analyses of thermally loaded structures.

Item URL in elib:https://elib.dlr.de/85325/
Document Type:Conference or Workshop Item (Speech)
Title:Comparison of Finite Element analysis and experimental results of a combustion chamber type TMF panel test
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Riccius, JörgUNSPECIFIEDhttps://orcid.org/0000-0002-5935-874X138948903
Journal or Publication Title:Proceedings
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:CFD, rocket engine, combustion
Event Title:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Event Location:San Jose, CA, USA
Event Type:international Conference
Event Start Date:14 July 2013
Event End Date:17 July 2013
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 - Antriebsystemtechnik - Schubkammertechnologie (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:22 Nov 2013 08:52
Last Modified:24 Apr 2024 19:51

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