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Shock interference peak heating measurements using phase change coatingsThe phase change coating technique is used to obtain peak heating measurements in shock interference flow regions with high surface shear and heating. This technique provides heat transfer coefficients which are determined by measuring the time for a point on the surface to reach the phase change temperature of the thin fusible coating. Measurements were conducted on a 5.08-cm diameter hemisphere-cylinder made of silica based epoxy at Mach 6 for free stream Reynolds numbers of 3.3 to 25.6 million per meter. A sketch of the shock interference pattern produced by a flat plate shock generator is included. Heating data obtained on a 5.08-cm diameter stainless steel hemispherical model instrumented with thermocouples is presented for the purpose of comparing the phase change technique with the thermocouple-calorimeter technique.
Document ID
19760043605
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Keyes, J. W.
(NASA Langley Research Center High-Speed Aerodynamic Div., Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 13
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
76A26571
Distribution Limits
Public
Copyright
Other

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