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Effect of ablation product absorption and line transitions on shock layer radiative transportAblation product absorption and line transitions effects on shock layer radiative transport around blunt body
Document ID
19690009779
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hoshizaki, H. (Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Wilson, K. H. (Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
August 5, 2013
Publication Date
February 1, 1969
Publication Information
Publisher: NASA
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-1264
Report Number: NASA-CR-1264
Accession Number
69N19117
Funding Number(s)
CONTRACT_GRANT: NAS7-509
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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