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Validation of the FLOWer-Code for Aerodynamics of Capsules

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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Abstract

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.

Item URL in elib:https://elib.dlr.de/36420/
Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1996,
Title:Validation of the FLOWer-Code for Aerodynamics of Capsules
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Giese, P.UNSPECIFIEDUNSPECIFIED
Longo, J.M.A.UNSPECIFIEDUNSPECIFIED
Date:1996
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:17
Status:Published
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: DLR-Beauftragter, elib
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:06

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