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Modifications to the DLR High Enthalpy Shock Tunnel HEG for Measurements on Supersonic Combustion

Beck, Walter and Hannemann, Klaus and Weiland, Matthias (2001) Modifications to the DLR High Enthalpy Shock Tunnel HEG for Measurements on Supersonic Combustion. American Institute of Aeronautics & Astronautics. 10th International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan, 24. - 27. Apr. 2001. DOI: 10.2514/6.2001-1860

Full text not available from this repository.

Official URL: http://arc.aiaa.org/doi/pdf/10.2514/6.2001-1860

Abstract

World-wide interest in attaining cheaper access to space by developing technologies such as supersonic combustion (SCRAMJET) engines, coupled with the degree of activity in ground-testing of the pertinent physical phenomena, have led to a decision to modify the existing DLR High Enthalpy Shock Tunnel (HEG) to provide full simulation conditions for flight at Mach 8 at an altitude of 27 kilometers. A design study has shown that a new shorter contoured nozzle will be needed, leading also to modifications in the existing test section and optical diagnostics placement. The new tunnel run parameters (piston trajectory) and the new low enthalpy (-3 MJ kg'1) conditions will also need to be calibrated.

Item URL in elib:https://elib.dlr.de/81530/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Modifications to the DLR High Enthalpy Shock Tunnel HEG for Measurements on Supersonic Combustion
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Beck, WalterUNSPECIFIEDUNSPECIFIED
Hannemann, KlausUNSPECIFIEDUNSPECIFIED
Weiland, MatthiasUNSPECIFIEDUNSPECIFIED
Date:2001
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2001-1860
Page Range:pp. 1-8
Editors:
EditorsEmail
AIAA, UNSPECIFIED
Publisher:American Institute of Aeronautics & Astronautics
Series Name:Conference Proceedings online
Status:Published
Keywords: DLR High Enthalpy Shock Tunnel (HEG), supersonic combustion, simulation conditions
Event Title:10th International Space Planes and Hypersonic Systems and Technologies Conference
Event Location:24. - 27. Apr. 2001
Event Type:international Conference
Event Dates:Kyoto, Japan
Organizer:American Institute of Aeronautics & Astronautics
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 - Raumfahrzeugsysteme - Anlagen u. Messtechnik
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Micknaus, Ilka
Deposited On:19 Apr 2013 11:59
Last Modified:19 Apr 2013 11:59

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