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Pressure Distribution and Stanton Number Distribution Measurement on a Hyperboloid-Flare Model at M &#61 8.7.

Niezgodka, J. and Henckels, A. (1994) Pressure Distribution and Stanton Number Distribution Measurement on a Hyperboloid-Flare Model at M &#61 8.7. DLR-Interner Bericht. 39113-94C07, 63 S.

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Abstract

In the hypersonic wind tunnel H2K of the DLR in Cologne tests have been performed with an axisymmetric hyperboloid-flare model at a Mach number M &#61 8.7 and Reynolds numbers Re &#61 35640 and 71280 related to the model length L &#61 59.404 mm. This hyperboloid-flare contour has been defined within the ESA/CNES technical assistance programme as one test case dealing with a large separation area and its dependence on laminar viscous interaction parameter M / Re. Pressure distribution has been measured as well as Stanton number distribution using thin wall technique with individual thermocouples and thick wall technique with infrared thermography.

Document Type:Monograph (DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1994,
Title:Pressure Distribution and Stanton Number Distribution Measurement on a Hyperboloid-Flare Model at M &#61 8.7.
Authors:
AuthorsInstitution or Email of Authors
Niezgodka, J.UNSPECIFIED
Henckels, A.UNSPECIFIED
Date:1994
Number of Pages:63
Status:Published
Keywords:Hyperboloid-flare, Pressure Distribution, Stanton Number Distribution, Thin Wall Technique, Thick Wall Technique, Infrared Thermography, Laminar Boundary Layer Separation
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):UNSPECIFIED
Location: Köln-Porz
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology
Deposited By: elib DLR-Beauftragter
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:27

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