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Stagnation-point solutions for an inviscid, radiating shock layer.Solutions indicating Boltzmann and Bueger numbers effect on radiant heat transfer and shock standoff distance for inviscid radiating shock layer
Document ID
19650042960
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Olstad, W. B.
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-RP-599
Report Number: NASA-RP-599
Accession Number
65A25664
Distribution Limits
Public
Copyright
Other
Keywords
STAGNATION POINT
SHOCK LAYER
RADIATIVE HEAT TRANSFER

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