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The effects of shock layer radiation and viscous coupling on the total heating rate to a reentering blunt bodyCoupling radiative and convective heat transfer in hypersonic blunt body reentry
Document ID
19680016334
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Engel, C. D. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Spradley, L. W. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
August 4, 2013
Publication Date
April 1, 1968
Publication Information
Publisher: NASA
Subject Category
Thermodynamics And Combustion
Report/Patent Number
LMSC/HREC-A791241
NASA-CR-61224
Report Number: LMSC/HREC-A791241
Report Number: NASA-CR-61224
Accession Number
68N25806
Funding Number(s)
CONTRACT_GRANT: NAS8-20082
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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