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BOUNDARY-LAYER CHANGES ACROSS AN INCIDENT REFLECTING SHOCKCalculation of changes in thickness and velocity profiles imposed on a turbulent boundary layer by the action of an incident reflecting oblique shock
Document ID
19630021475
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Pinckney, S. Z.
Date Acquired
August 1, 2013
Publication Date
April 25, 1963
Subject Category
Facilities, Research, And Support
Report/Patent Number
AIAA PAPER 63116
Report Number: AIAA PAPER 63116
Accession Number
63A17534
Distribution Limits
Public
Copyright
Other
Keywords
BOUNDARY LAYER FLOW
TURBULENT BOUNDARY LAYER
SHOCK WAVE INTERACTION
OBLIQUE SHOCK WAVE

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