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Comparison of supersonic combustion tests with shock tunnels, flight and CFD

Steelant, Johan and Mack, Andreas and Hannemann, Klaus and Gardner, Anthony Donald (2006) Comparison of supersonic combustion tests with shock tunnels, flight and CFD. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 9-12, 2006, Sacramento, California.

Full text not available from this repository.

Abstract

In 2002, the HyShot flight experiment was sucessfully launched and allowed to access experimental flight data for supersonic combustion. Ground based testing performed in the High Enthalpy Shock Tunnel (HEG) of the German Aerospace Center (DLR) allowed to reproduce the Mach 7.8 conditions. The present numerical work focuses on the computation of the experiments in the HEG considering flows with and without combustion and fuel injection. Further, variations of the equivalence ratio and the resulting influence on the flow topology are studied.

Item URL in elib:https://elib.dlr.de/48948/
Document Type:Conference or Workshop Item (Paper)
Title:Comparison of supersonic combustion tests with shock tunnels, flight and CFD
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Steelant, JohanESA-ESTECUNSPECIFIED
Mack, AndreasESA-ESTECUNSPECIFIED
Hannemann, KlausUNSPECIFIEDUNSPECIFIED
Gardner, Anthony DonaldUNSPECIFIEDUNSPECIFIED
Date:2006
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Series Name:AIAA-2006-4684
Status:Published
Keywords:scramjet, HEG, hypersonic, HyShot, CFD, TAU, combustion, hydrogen, turbulence, mixing, crossflow injection
Event Title:42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Event Location:Sacramento, California
Event Type:international Conference
Event Dates:July 9-12, 2006
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W - no assignment
DLR - Research area:Space
DLR - Program:W - no assignment
DLR - Research theme (Project):W - no assignment (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Gardner, Dr.habil. Anthony
Deposited On:25 Jun 2007
Last Modified:27 Apr 2009 13:52

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