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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 (2006) Comparison of Supersonic Combustion Tests with Shock Tunnels Flight and CFD. In: AIAA Conference Proceedings, Session 60-HYP-3 (AIAA 2006-4684), p. 14. American Institute of Aeronautics and Astronautics. 42th AIAA Joint Propulsion Conference, 2006-07-09 - 2006-07-12, Sacramento, CA (USA).

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Official URL: http://www.aiaa.org/content.cfm?pageid=320


In 2002, the HyShot supersonic flight experiment was successfully 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 flight conditions. The present numerical work focuses on the computation of the experiments in 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/44288/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Comparison of Supersonic Combustion Tests with Shock Tunnels Flight and CFD
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Steelant, JohanESTEC, ESA, 2200 AG Noordwijk, NLUNSPECIFIED
Mack, AndreasESTEC, ESA, 2200 AG Noordwijk, NLUNSPECIFIED
Journal or Publication Title:AIAA Conference Proceedings
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Volume:Session 60-HYP-3
Page Range:p. 14
Publisher:American Institute of Aeronautics and Astronautics
Series Name:Conference Proceedings CD/Online
Keywords:scramjet, HEG, hypersonic
Event Title:42th AIAA Joint Propulsion Conference
Event Location:Sacramento, CA (USA)
Event Type:international Conference
Event Dates:2006-07-09 - 2006-07-12
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 - Grundlagen Raumtransport - Anlagen und Messtechnik (old)
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Brennecke-Hosseinzadeh, Dagmar
Deposited On:29 Aug 2007
Last Modified:14 Jan 2010 23:08

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