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Ground testing of the HyShot II Scramjet Configuration in HEG

Martinez Schramm, Jan and Karl, Sebastian and Hannemann, Klaus and Steelant, Johan (2008) Ground testing of the HyShot II Scramjet Configuration in HEG. 15th AIAA Int. Space Planes and Hypersonic Systems and Technology Conference, 2008-04-28 - 2008-05-01, Dayton, OH (USA).

Full text not available from this repository.

Abstract

Ground based testing of the HyShot II supersonic combustion ramjet flight configuration was carried out in the High Enthalpy Shock Tunnel Göttingen, HEG, of the German Aerospace Center, DLR. The main focus of these investigations was to obtain surface pressure and surface heat transfer data on the intake and the cowl and body side surfaces of the combustion chamber and the nozzle. Further, high speed flow visualisation of the combustor flow was performed. Two HEG operating conditions which are related to 33km and 27km flight altitude were applied. Computational fluid dynamics (CFD) was applied to support the analysis of the experimental results and for the prediction of the free stream conditions in the HEG test section.

Document Type:Conference or Workshop Item (Speech)
Title:Ground testing of the HyShot II Scramjet Configuration in HEG
Authors:
AuthorsInstitution or Email of Authors
Martinez Schramm, JanUNSPECIFIED
Karl, SebastianUNSPECIFIED
Hannemann, KlausUNSPECIFIED
Steelant, JohanESA-ESTEC
Date:2008
Refereed publication:No
In SCOPUS:No
In ISI Web of Science:No
Status:Accepted
Keywords:Scramjet, HEG, Hypersonics
Event Title:15th AIAA Int. Space Planes and Hypersonic Systems and Technology Conference
Event Location:Dayton, OH (USA)
Event Type:international Conference
Event Dates:2008-04-28 - 2008-05-01
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W - no assignement
DLR - Research area:Space
DLR - Program:W - no assignement
DLR - Research theme (Project):W -- no assignement (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Dagmar Brennecke-Hosseinzadeh
Deposited On:10 Jul 2008
Last Modified:27 Apr 2009 14:55

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