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The structure of the viscous hypersonic shock layerUnified theoretical model of hypersonic viscous shock layer for wide range of Reynolds numbers, including mass transfer effects
Document ID
19660006945
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Goldberg, L. (General Electric Co. Philadelphia, PA, United States)
Date Acquired
August 3, 2013
Publication Date
December 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-69831
R65SD50
Report Number: NASA-CR-69831
Report Number: R65SD50
Accession Number
66N16234
Funding Number(s)
CONTRACT_GRANT: SNPC-29
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VISCOUS FLOW
SHOCK LAYER
HYPERSONIC SHOCK
MASS TRANSFER
MATHEMATICAL MODEL

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