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Experiments on Shock-Boundary Layer Interaction and Cooling Efficiency in a Transpiration Cooled Model Scramjet

Strauss, Friedolin and Witte, Jan and Weißwange, Matthias and Manfletti, Chiara and Schlechtriem, Stefan (2017) Experiments on Shock-Boundary Layer Interaction and Cooling Efficiency in a Transpiration Cooled Model Scramjet. In: 53rd AIAA/SAE/ASEE Joint Propulsion Conference. 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 10.-12. Jul. 2017, Atlanta, GA, USA. doi: 10.2514/6.2017-4833.

Full text not available from this repository.

Official URL: https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4833


Transpiration cooling systems are a promising approach to handle the high wall temperatures and heat loads generated in supersonic combustion ramjets (scramjets). The German Aerospace Center DLR has conducted experiments to investigate the applicability of transpiration cooling systems in scramjets and the phenomena resulting out of the interaction between a wedge/ flame holder and coolant secondary flow. Results with nitrogen as coolant for different sintered porous materials, different blowing ratios and different boundary conditions with and without wedge are shown. A detailed analysis using i.a. optical Schlieren investigations is presented. Phenomena like choking and shock-coolant plenum feedback are addressed. Further research is discussed and concretized.

Item URL in elib:https://elib.dlr.de/116711/
Document Type:Conference or Workshop Item (Speech)
Title:Experiments on Shock-Boundary Layer Interaction and Cooling Efficiency in a Transpiration Cooled Model Scramjet
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Strauss, Friedolinfriedolin.strauss (at) dlr.dehttps://orcid.org/0000-0002-1385-4326
Witte, JanJan.Witte (at) dlr.deUNSPECIFIED
Weißwange, MatthiasMatthias.Weisswange (at) dlr.deUNSPECIFIED
Manfletti, Chiarachiara.manfletti (at) esa.intUNSPECIFIED
Schlechtriem, Stefanstefan.schlechtriem (at) dlr.deUNSPECIFIED
Date:10 July 2017
Journal or Publication Title:53rd AIAA/SAE/ASEE Joint Propulsion Conference
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
DOI :10.2514/6.2017-4833
Keywords:Transpiration Cooling, Scramjet, Flow Interaction, Supersonic Flow, Shock-Boundary Layer Interaction
Event Title:53rd AIAA/SAE/ASEE Joint Propulsion Conference
Event Location:Atlanta, GA, USA
Event Type:international Conference
Event Dates:10.-12. Jul. 2017
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 - Raketenantriebtests (old), R - Antriebsystemtechnik - Schubkammertechnologie (old), R - Reusable Space Systems and Propulsion Technology
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Institute of Space Propulsion > Propellants
Deposited By: Strauss, Friedolin
Deposited On:06 Dec 2017 15:48
Last Modified:06 Dec 2017 15:48

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