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Transitional and turbulent heat transfer correlations for a lifting entry vehicle at Mach 10Applicability of boundary layer transition and turbulent heat transfer data for lifting reentry vehicle at hypersonic speed to space shuttles
Document ID
19700028526
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Reda, D. C. (General Dynamics/Convair San Diego, CA, United States)
Roberge, A. M. (General Dynamics/Convair San Diego, CA, United States)
Young, C. H. (General Dynamics/Convair San Diego, CA, United States)
Date Acquired
August 5, 2013
Publication Date
July 1, 1970
Publication Information
Publication: NASA, WASHINGTON SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 1 JUL. 1970
Subject Category
Thermodynamics And Combustion
Accession Number
70N37842
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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