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CFD Analysis of the HyShot Scramjet Configuration

Karl, Sebastian (2007) CFD Analysis of the HyShot Scramjet Configuration. 13. STAB-Workshop, 2007-11-14 - 2007-11-15, Göttingen. (Unpublished)

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Abstract

Testing of the HyShot II scramjet configuration was carried out in the High Enthalpy Shock Tunnel Goettingen, HEG. Computational fluid dynamics (CFD) is applied to support the analysis of experimental results and for the prediction of the free stream conditions in the HEG test section. Numerical simulations of the flow in the complete HyShot configuration for fuel on and off conditions were performed.

Item URL in elib:https://elib.dlr.de/51975/
Document Type:Conference or Workshop Item (Speech)
Title:CFD Analysis of the HyShot Scramjet Configuration
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Karl, SebastianUNSPECIFIEDUNSPECIFIED
Date:2007
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:Scramjet, HEG, CFD
Event Title:13. STAB-Workshop
Event Location:Göttingen
Event Type:Other
Event Dates:2007-11-14 - 2007-11-15
Organizer:DLR Göttingen
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: Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Brennecke-Hosseinzadeh, Dagmar
Deposited On:14 Jan 2008
Last Modified:27 Apr 2009 14:30

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