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.

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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:

Authors	Institution or Email of Authors
Hannemann, Klaus
Karl, Sebastian
Martinez Schramm, Jan
Laurence, Stuart

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:

Raumfahrt

HGF - Program Themes:

R RP - Raumtransport

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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