High Enthalpy Testing and CFD Rebuilding of X-38 in HEG
Hannemann, K. and Schramm, J.M. and Brück, S. and Longo, J.M.A. (2001) High Enthalpy Testing and CFD Rebuilding of X-38 in HEG. 4th Symposium on Aerothermodynamics for Space Vehicles, Capua (it), 14.-18.10.2001.
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Ground based testing of X-38 was performed in the High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center (DLR). Parallel to this testing program Computational Fluid Dynamics (CFD) rebuilding was employed using the DLR Navier-Stokes solver CEVCATS-N. The Model E, which is a 1:24 scaled wind tunnel model of the X-38 vehicle, was used to obtain the first surface heat flux and pressure measurements of this configuration in the high enthalpy flow regime. Two different HEG operating conditions with total enthalpies of 12MJ/kg and 22MJ/kg were used.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||High Enthalpy Testing and CFD Rebuilding of X-38 in HEG|
|Keywords:||Re-entry, hypersonic, CFD, wind tunnel, real gas|
|Event Title:||4th Symposium on Aerothermodynamics for Space Vehicles, Capua (it), 14.-18.10.2001|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Space|
|HGF - Program Themes:||W RP - Raumtransport|
|DLR - Research area:||Space|
|DLR - Program:||W RP - Raumtransport|
|DLR - Research theme (Project):||W - Grundlagen Raumtransport - Anlagen und Messtechnik (old)|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology|
|Deposited By:||Claudia Grant|
|Deposited On:||31 Jan 2006|
|Last Modified:||14 Jan 2010 18:53|
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