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The leading-edge effects on the laminar flat- plate boundary layer and the aerodynamic heating at Mach 10.4Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.4
Document ID
19690014093
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Stone, H. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1969
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-5160
Report Number: NASA-TN-D-5160
Accession Number
69N23467
Funding Number(s)
CONTRACT_GRANT: 129-01-07-07-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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