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Heat-transfer measurements and computations of swept-shock-wave boundary-layer interactionsAn experimental and computational research program providing new knowledge of the heat transfer in swept-shock-wave/boundary-layer interactions is described. An equilibrium turbulent boundary layer on a flat plate is subjected to impingement by a swept planar shock wave generated by a sharp fin. Five different interactions with fin angles ranging from 10 to 20 deg at freestream Mach numbers of 3 and 4 produce a variety of interaction strengths ranging from weak to very strong. A foil heater generates a uniform heat flux over the flat plate surface, and miniature thin-film-resistance sensors are used to measure the local surface temperature. The heat convection equation is then solved for the heat transfer distribution within an interaction, yielding an uncertainty of about +/- 10%. These data are compared with numerical Navier-Stokes solutions that employ a k-epsilon turbulence model. A simple peak heat transfer correlation for fin interactions is suggested.
Document ID
19950056083
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Lee, Y.
(Penn Sate Univ. University Park, PA, United States)
Settles, G. S.
(Penn Sate Univ. University Park, PA, United States)
Horstman, C. C.
(NASA Ames Research Center Moffet Field, CA, United States)
Date Acquired
August 16, 2013
Publication Date
April 1, 1994
Publication Information
Publication: AIAA Journal
Volume: 32
Issue: 4
ISSN: 0001-1452
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
95A87682
Funding Number(s)
CONTRACT_GRANT: NAG2-592
Distribution Limits
Public
Copyright
Other

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