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Shock interference heating and density ratio effects. Part 2 - Hypersonic density ratio effectsHypersonic shock/density ratio effects in aerothermodynamic heating of space shuttle configuration
Document ID
19710016582
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Creel, T. R., Jr. (NASA Langley Research Center Hampton, VA, United States)
Hunt, J. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 6, 2013
Publication Date
April 1, 1971
Publication Information
Publication: NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 1 APR. 1971
Subject Category
Thermodynamics And Combustion
Accession Number
71N26058
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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