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An analysis of the coupled chemically reacting boundary layer and charring ablator. Part 3 - Nonsimilar solution of the multicomponent laminar boundary layer by an integral matrix methodLaminar boundary layer problems solved by integral matrix methods
Document ID
19680017169
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bartlett, E. P. (Aerotherm Corp. Palo Alto, CA, United States)
Kendall, R. M. (Aerotherm Corp. Palo Alto, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1968
Publication Information
Publisher: NASA
Subject Category
Thermodynamics And Combustion
Report/Patent Number
REPT.-66-7, PT. 3
NASA-CR-1062
Report Number: REPT.-66-7, PT. 3
Report Number: NASA-CR-1062
Accession Number
68N26641
Funding Number(s)
CONTRACT_GRANT: NAS9-4599
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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