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Further studies of the coupled chemically reacting boundary layer and charring ablator. Part 4 - Nonsimilar solution of an incompressible turbulent boundary layer by an integral matrix methodNonsimilar solution of incompressible turbulent boundary layer by integral matrix method
Document ID
19690008460
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Anderson, L. W. (Aerotherm Corp. Palo Alto, CA, United States)
Kendall, R. M. (Aerotherm Corp. Palo Alto, CA, United States)
Date Acquired
August 5, 2013
Publication Date
October 15, 1968
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-92474
REPT-68-38-PT-4
Report Number: NASA-CR-92474
Report Number: REPT-68-38-PT-4
Accession Number
69N17792
Funding Number(s)
CONTRACT_GRANT: NAS9-6719
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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