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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.
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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/ | ||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech, Paper) | ||||||||||||||||
| Title: | Modifications to the DLR High Enthalpy Shock Tunnel HEG for Measurements on Supersonic Combustion | ||||||||||||||||
| Authors: |
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| 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: |
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| 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 Transportation | ||||||||||||||||
| DLR - Research area: | Raumfahrt | ||||||||||||||||
| DLR - Program: | R RP - Space Transportation | ||||||||||||||||
| DLR - Research theme (Project): | R - Raumfahrzeugsysteme - Anlagen u. Messtechnik (old) | ||||||||||||||||
| 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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