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Aerodynamic heat transfer to RSI tile surfaces and gap intersectionsReview of the results of aerothermal heating tests of a simulated reusable surface insulation (RSI) tile array, performed on the sidewall of a Mach-10 hypersonic tunnel. In particular, the heating characteristics of the tile array, such as they result from heating inside the tile-expansion-space providing gaps between individual tiles, are investigated. The results include the finding that heating on the upstream face of a tile is strongly affected by the interacting longitudinal gap flow.
Document ID
19740049624
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Dunavant, J. C.
Throckmorton, D. A.
(NASA Langley Research Center Space Systems Div., Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
June 1, 1974
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 11
Subject Category
Thermodynamics And Combustion
Accession Number
74A32374
Distribution Limits
Public
Copyright
Other

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