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Methodology of a Combined Ground Based Testing and Numerical Modelling Analysis of Supersonic Combustion Flow Paths

Hannemann, Klaus and Karl, Sebastian and Martinez Schramm, Jan and Laurence, Stuart (2011) Methodology of a Combined Ground Based Testing and Numerical Modelling Analysis of Supersonic Combustion Flow Paths. Conference of Aeronautical Society of the Republic of China & Aerospace Research Program of National Science Council, 05.11.2011, Taichung, Taiwan.

Full text not available from this repository.

Abstract

DLR in General – Göttingen DLR Site Scramjet Research - Motivation, Methodology HyShot Flight Experiment High Enthalpy Shock Tunnel Göttingen, HEG DLR TAU Code HyShot II Results (ground based testing in HEG and CFD) Summary and Conclusions

Document Type:Conference or Workshop Item (Speech)
Title:Methodology of a Combined Ground Based Testing and Numerical Modelling Analysis of Supersonic Combustion Flow Paths
Authors:
AuthorsInstitution or Email of Authors
Hannemann, KlausUNSPECIFIED
Karl, SebastianUNSPECIFIED
Martinez Schramm, JanUNSPECIFIED
Laurence, StuartUNSPECIFIED
Date:November 2011
Status:Published
Keywords:Scramjet, HyShot, HEG, DLR TAU
Event Title:Conference of Aeronautical Society of the Republic of China & Aerospace Research Program of National Science Council
Event Location:Taichung, Taiwan
Event Type:international Conference
Event Dates:05.11.2011
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - EU Projekte Raumtransport
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Dagmar Brennecke-Hosseinzadeh
Deposited On:17 Jan 2012 12:09
Last Modified:17 Jan 2012 12:09

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