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Use of fusible temperature indicators for obtaining quantitative aerodynamic heat-transfer dataFusible thin film coatings used in determining aerodynamic heat transfer coefficients at hypersonic speeds
Document ID
19660006873
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Hunt, J. L. (NASA Langley Research Center Hampton, VA, United States)
Jones, R. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TR-R-230
Report Number: NASA-TR-R-230
Accession Number
66N16162
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THIN FILM
AERODYNAMIC HEAT TRANSFER
HYPERSONIC SPEED
HEAT-TRANSFER COEFFICIENT

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