ARD Post-Flight Analysis , Numerical Simulation and Experiments at HEG
Weiland, M.K.H. and Johnston, I.A. and Martinez Schramm, J. and Hannemann, K. (2001) ARD Post-Flight Analysis , Numerical Simulation and Experiments at HEG. DLR-Interner Bericht. 223-2001 A 10, 77 S.
Full text not available from this repository.
A postflight investigation of the hypersonic aerothermodynamics of the European Space Agency's Atmospheric Reentry Demonstrator (ARD) has been undertaken by DLR under EADS-LV contract. As part of the investigation, experimental work was conducted on a scale-model of the capsule in the HEG shock tunnel and, in parallel, computational fluid dynamics simulations of the experiment were produced. Presented in this report are descriptions of the numerical and experimental techniques, and results for heat transfer and pressure distributions over the model. We particularly focus on the integration of numerical and experimental methods as a way to improve results, and to help uncover and overcome deficiencies inherent to both techniques. Numerical simulation is also used to gauge the effects of nonuniformity and high-temperature flow processes in the shock-tunnel test flow.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||ARD Post-Flight Analysis , Numerical Simulation and Experiments at HEG|
|Number of Pages:||77|
|Keywords:||Hypersonic aerothermodynamics, scale-model of the capsule in the HEG shock tunnel.|
|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:||elib DLR-Beauftragter|
|Deposited On:||31 Jan 2006|
|Last Modified:||14 Jan 2010 18:49|
Repository Staff Only: item control page