Giese, P. and Longo, J.M.A. (1996) Validation of the FLOWer-Code for Aerodynamics of Capsules. DLR-Interner Bericht. 129-96/35, 17 S.
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Numerical flow simulations around a biconic capsule under inviscid supersonic and hypersonic flow conditions are presented and discussed. The numerical solutions are performed with the DLR FLOWer-code for a range of angles of attack upto 60*. The accuracy of the solutions are addressed through out grid convergence studies and comparing results with solutions obtained with the CEVCATS-code, as well as with available experimental data. The results indicate a qualitative and quantitative good agreement between the numerical solutions performed with both computer codes. Also, the comparison of computed aerodynamic coefficients with experimental data shows a very good correlation. However, the tested version of the FLOWer- code is not suitable for engineering applications in supersonic and hypersonic flow problems. Since it is based on a central differencing scheme its rates of convergence are very poor when comparing with the upwind scheme of the CEVCATS-code. The present.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||Validation of the FLOWer-Code for Aerodynamics of Capsules|
|Number of Pages:||17|
|Keywords:||Supersonic flow, hypersonic flow, capsule aerodynamic, inviscid flow, numerical simulation|
|HGF - Research field:||UNSPECIFIED|
|HGF - Program:||Space (old)|
|HGF - Program Themes:||W RP - Raumtransport|
|DLR - Research area:||UNSPECIFIED|
|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 > Institut für Entwurfsaerodynamik|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||03 Apr 2006|
|Last Modified:||27 Apr 2009 10:06|
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