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Contribution of Aerodynamics for Future SCT

Herrmann, U. and Orlowski, M. and Radespiel, R. (1998) Contribution of Aerodynamics for Future SCT. In: Computational Fluid Dynamics 1998, Volume 2, pp. 649-654. John Wiley & Sons, Ltd.. ECCOMAS, Athen (gr), 07.-11.09.1998.

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Abstract

The validation of the DLR Navier-Stokes solver for aerodynamics prediction of Supersonic Commercial Transport (SCT) is reviewed. Aeroelastic effects in supersonic flow experiment are demonstrated numerically. Mesh density and turbulence model effects on flow topology and aerodynamic coefficients at transonic and subsonic speeds are described. The potential of aerodynamic optimization is demonstrated by typical generic SCT applications at supersonic cruise conditions.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1999,
Title:Contribution of Aerodynamics for Future SCT
Authors:
AuthorsInstitution or Email of Authors
Herrmann, U.UNSPECIFIED
Orlowski, M.UNSPECIFIED
Radespiel, R.UNSPECIFIED
Date:1998
Journal or Publication Title:Computational Fluid Dynamics 1998
Volume:Volume 2
Page Range:pp. 649-654
Editors:
EditorsEmail
Papailiou, K.D.UNSPECIFIED
Tshahalis, D.UNSPECIFIED
Périaux, J.UNSPECIFIED
Knörzer, D.UNSPECIFIED
Publisher:John Wiley & Sons, Ltd.
Status:Published
Keywords:supersonic transport, numerical flow simulation, aerodynamic optimization, code validation, vortex flow, aeroelastic effects, low speed flow
Event Title:ECCOMAS, Athen (gr), 07.-11.09.1998
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):L - Concepts & Integration
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: Claudia Grant
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 19:57

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