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Force and Heat Transfer on a Delta Wing in Rarefied Flow

Legge, H. (1992) Force and Heat Transfer on a Delta Wing in Rarefied Flow. In: Vorgesehen zur Veröffentlichung in: Workshop on Hypersonic Flows for Reentry Problems, Part II. Springer-Verlag. Springer - Verlag Berlin.

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Abstract

For testing numerical methods in the rearefied regime a broad range in parameter variation, especially in the Knudsen number is advisable. Therefore the drag, lift total heat transfer and recovery temperatureof a small delta wing (5mm length) was tested in a sonic orifice free jet flow. In this report the experimental technique and the main results will be given. Details are given in Ref.1 where also different correlation parameters are examined by comparing experimental and theoretical results, especially of the workshops in Antibes 1990 and 1991.

Document Type:Conference or Workshop Item (Paper)
Additional Information: institution=R. Abgrall, J.A. Desideri, R. Glowinski, M. Mallet, J. Periaux, LIDO-Berichtsjahr=1992, pages=12,
Title:Force and Heat Transfer on a Delta Wing in Rarefied Flow
Authors:
AuthorsInstitution or Email of Authors
Legge, H.UNSPECIFIED
Date:1992
Journal or Publication Title:Vorgesehen zur Veröffentlichung in: Workshop on Hypersonic Flows for Reentry Problems, Part II. Springer-Verlag
Publisher:Springer - Verlag Berlin
Status:Published
Keywords:Delta wing, drag, lift, heat transfer, recovery temperatur, rarefied hypersonic flow.
HGF - Research field:UNSPECIFIED
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:no assignment
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik > Institut für Experimentelle Strömungsmechanik
Deposited By: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:07

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