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Ground Testing of the HyShot Supersonic Combustion Flight Experiment in HEG

Gardner, Anthony and Hannemann, Klaus and Paull, Alan and Steelant, Johan (2004) Ground Testing of the HyShot Supersonic Combustion Flight Experiment in HEG. 24th International Symposium on Shock Waves, 2004-07-11 - 2004-07-16, Beijing, CHINA. ISBN 3-540-22497-1.

Full text not available from this repository.

Abstract

The scramjet geometry used for the HyShot flight tests was tested with 1:1 scaling in the HEG shock tunnel at test conditions corresponding to Mach 7.8 flight at 28km and 33km altitude. The paper compares pressure distributions over the model with those taken in flight, and shows heat flux distributions.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2004,
Title:Ground Testing of the HyShot Supersonic Combustion Flight Experiment in HEG
Authors:
AuthorsInstitution or Email of Authors
Gardner, AnthonyUNSPECIFIED
Hannemann, KlausUNSPECIFIED
Paull, AlanUniversity Queensland
Steelant, JohanESA-ESTEC
Date:2004
Page Range:pp. 329-334
Editors:
EditorsEmail
Jiang, Z.UNSPECIFIED
ISBN:3-540-22497-1
Status:Published
Keywords:HyShot, Scramjet, HEG, hypersonic, flight-testing, combustion
Event Title:24th International Symposium on Shock Waves
Event Location:Beijing, CHINA
Event Type:international Conference
Event Dates:2004-07-11 - 2004-07-16
Organizer:Institute of Mechanics Chinese Academy of Sciences
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 - numerische Verfahren (old)
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Dagmar Brennecke-Hosseinzadeh
Deposited On:17 Feb 2006
Last Modified:27 Apr 2009 04:56

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