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Investigation of Film Cooling Efficiency in a High Pressure Subscale LOX/H2 Combustion Chamber

Suslov, Dmitry and Haidn, Oskar and Arnold, R. (2011) Investigation of Film Cooling Efficiency in a High Pressure Subscale LOX/H2 Combustion Chamber. In: Proceedings (AIAA 2011-5778). 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 31. Jul. - 3. Aug. 2011, San Diego, California, U´SA.

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Abstract

Film cooling performance in a LOX/H2 subscale combustion chamber was investigated. This paper presents both a new test specimen and measurement technique, developed and successfully tested by the Institute of Space Propulsion, as well as experimental results. The new measurement method provides detailed information about the cooling film efficiency and thermal load distribution on the hot inner surfaces at real rocket engine conditions and pressures up to 11.5 MPa. The presented investigations have been performed at the European Research and Technology Test Facility.

Item URL in elib:https://elib.dlr.de/72138/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Investigation of Film Cooling Efficiency in a High Pressure Subscale LOX/H2 Combustion Chamber
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Suslov, DmitryDmitry.Suslov (at) dlr.deUNSPECIFIED
Haidn, OskarOskar.Haidn (at) dlr.deUNSPECIFIED
Arnold, R.Astrium OttobrunnUNSPECIFIED
Date:August 2011
Journal or Publication Title:Proceedings
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:film cooling, combustion
Event Title:47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Event Location:San Diego, California, U´SA
Event Type:international Conference
Event Dates:31. Jul. - 3. Aug. 2011
Organizer:AIAA
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):W - Antriebsystemtechnik - Schubkammertechnologie und Hochdruckverbrennung (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Institute of Space Propulsion > Technologie
Deposited By: Hanke, Michaela
Deposited On:30 Nov 2011 11:59
Last Modified:01 Dec 2018 19:47

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