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Sensitivity Analysis for the HyShot Generic Supersonic Combustion Configuration using CFD

Mack, Andreas and Steelant, Johan and Martinez Schramm, Jan and Hannemann, Klaus (2007) Sensitivity Analysis for the HyShot Generic Supersonic Combustion Configuration using CFD. In: Proceedings of XVIII Symposium on Air Breathing Engines. XVIII International Symposium on Airbreathing Engines (ISABE), 2007-09-02 - 2007-09-07, Peking, (China).

Full text not available from this repository.

Abstract

Numerical simulations for the HyShot configuration have been performed for the flow conditions of the 2007 measurement campaign. At an equivalence ratio of 0.3 numerical simulations for fuel on and off conditions were performed. Comparison is made with previous numerical solutions obtained on structured grids and the effect of different turbulence modeling is shown.

Item URL in elib:https://elib.dlr.de/52897/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Sensitivity Analysis for the HyShot Generic Supersonic Combustion Configuration using CFD
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Mack, AndreasESA-ESTECUNSPECIFIEDUNSPECIFIED
Steelant, JohanESA-ESTECUNSPECIFIEDUNSPECIFIED
Martinez Schramm, JanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Hannemann, KlausUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2007
Journal or Publication Title:Proceedings of XVIII Symposium on Air Breathing Engines
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Scramjet, CFD, Combustion
Event Title:XVIII International Symposium on Airbreathing Engines (ISABE)
Event Location:Peking, (China)
Event Type:international Conference
Event Start Date:2 September 2007
Event End Date:7 September 2007
Organizer:ISABE
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:15 Jan 2008
Last Modified:24 Apr 2024 19:16

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