HEG - A new shock tunnel for high enthalpies
Beck, W. and Eitelberg, G. and Vennemann, D. (1992) HEG - A new shock tunnel for high enthalpies. European Forum, Southampton University, 14.-17. Sept. 1992.
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HEG, a new high enthalpy shock tunnel has recently been inaugurated at DLR in Goettingen. Its prinicipal function within the aerodynamic strategy of the HERMES space vehicle project is to examine the influence of non-equilibrium gas dynamics on the external aerodynamics and heat fluxes of the vehicle in the range where heat loaads are highest. The facility layout of this free piston shock tunnel consists of three main sections, the driver section, the shocktube and the test section including a contoured nozzle. The main features of this arrangement are described along with a presentation of its main operaing characteristics. A description of the tunnel instrumentation focuses on the LIF system which is beeing developed and validated for use in HEG. Some validation results are presented. Finally the facility calibration procedure is described and first results are presented.
|Document Type:||Conference or Workshop Item (Speech)|
|Additional Information:||LIDO-Berichtsjahr=1992, pages=9,|
|Title:||HEG - A new shock tunnel for high enthalpies|
|Keywords:||High enthalpy shock tunnel, non-equilibrium gas dynamics, external aerodynamics, heat fluxes, free piston shock tunnel, LIF|
|Event Title:||European Forum, Southampton University, 14.-17. Sept. 1992|
|HGF - Research field:||UNSPECIFIED|
|HGF - Program:||no assignment|
|HGF - Program Themes:||no assignment|
|DLR - Research area:||UNSPECIFIED|
|DLR - Program:||no assignment|
|DLR - Research theme (Project):||UNSPECIFIED|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik > Institut für Experimentelle Strömungsmechanik|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||03 Apr 2006|
|Last Modified:||27 Apr 2009 10:07|
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