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Experimental stagnation point velocity gradients and heat transfer coefficients for a family of blunt bodies at Mach 8 and angles of attackStagnation pressure and heat transfer measurements of blunt axisymmetric bodies
Document ID
19690013192
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Ellison, J. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-5121
Report Number: NASA-TN-D-5121
Accession Number
69N22554
Funding Number(s)
CONTRACT_GRANT: 129-01-03-07-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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