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Subsonic Flow Around US-Orbiter Model FALKE in the DNW

Radespiel, R. (1994) Subsonic Flow Around US-Orbiter Model FALKE in the DNW. In: AGARD Advisory Report No. 303.

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Abstract

The contribution describes wind tunnel measurements of aerodynamic forces, pressure distributions and surface visualization for the FALKE model. FALKE is a model of the US-Orbiter in the scale 1:5.427. The test results taken in the subsonic wind tunnel DNW enable validation of computational methods for reentry vehicles in landing conditions at high Reynolds numbers, where strong vortical flow occurs in the upper side of the configuration.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1994, pages=13,
Title:Subsonic Flow Around US-Orbiter Model FALKE in the DNW
Authors:
AuthorsInstitution or Email of Authors
Radespiel, R.UNSPECIFIED
Date:1994
Journal or Publication Title:AGARD Advisory Report No. 303
Series Name:Paper E1
Status:Published
Keywords:Low speed, DNW, vortical flow, flow visualization, reentry vehicle
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 10:05

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