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Shock interference heating and density-ratio effects. Part 1 - Flow field visualization, thermocouple measurements, and analysisFlow visualization, thermocouple measurements, and analyses of shock interference heating effects on straight wing space shuttle model
Document ID
19710016581
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Seegmiller, H. L. (NASA Ames Research Center Moffett Field, CA, 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
71N26057
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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