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Thin radiating shock layer about a blunt bodyBoundary layer flow in thin shock layer about axisymmetric blunt bodies studied by Blasius type series expansion technique
Document ID
19700011439
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Blake, L. H. (Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Chou, Y. S. (Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
August 5, 2013
Publication Date
March 1, 1970
Publication Information
Publisher: NASA
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-1547
Report Number: NASA-CR-1547
Accession Number
70N20744
Funding Number(s)
CONTRACT_GRANT: NAS7-632
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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