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Integral method in compressible laminar boundary layers and its application.Properties of compressible boundary layers with heat transfer and arbitrary pressure gradients calculated, using integral equation and correlation concept for application in hypersonic flows
Document ID
19660045291
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Chan, Y.-Y.
Date Acquired
August 3, 2013
Publication Date
February 1, 1966
Subject Category
Fluid Mechanics
Accession Number
66A24581
Funding Number(s)
CONTRACT_GRANT: NSG-633
Distribution Limits
Public
Copyright
Other
Keywords
HYPERSONIC FLOW
PRESSURE GRADIENT
COMPRESSIBLE BOUNDARY LAYER
LAMINAR BOUNDARY LAYER
CORRELATION FUNCTION
INTEGRAL EQUATION
HEAT TRANSFER

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