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Investigations concerning wing-body interference for compressible flow

Wichmann, G. (1994) Investigations concerning wing-body interference for compressible flow. In: ICAS Proceedings 1994 Volume I, I, pp. 823-835. AIAA, Washington, USA. 19th Congress of the International Council of the Aeronautical Scienes, Anaheim, California, USA 18.-23.09.1994.

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Abstract

Numerical results concerning wing-body interference for compressible flow obtained by the use of an Euler method are presented. Beside the presentation of the basic mechanism of the mutual influence of wing and body there are pointed out the numerical results which had been obtained using simple principle models to determine the body effects and the Mach number effects on pressure and lift distributions of the configuration. A detailed analysis of the total lift behaviour of wing and body confirm the basic results.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1994,
Title:Investigations concerning wing-body interference for compressible flow
Authors:
AuthorsInstitution or Email of Authors
Wichmann, G.UNSPECIFIED
Date:1994
Journal or Publication Title:ICAS Proceedings 1994 Volume I
Volume:I
Page Range:pp. 823-835
Publisher:AIAA, Washington, USA
Status:Published
Keywords:Wing-body interference, body influence, Mach number influence, induced lift, lift ratio body/wing-body, sweep effects
Event Title:19th Congress of the International Council of the Aeronautical Scienes, Anaheim, California, USA 18.-23.09.1994
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
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: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:05

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