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Flow visualization experiments with separated supersonic turbulent flowShadowgraph and flow visualization wind tunnel test of supersonic flow mechanisms during turbulent separation of cylinder-flare
Document ID
19660021026
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lowson, M. V. (Wyle Labs., Inc. Huntsville, AL, United States)
Date Acquired
August 3, 2013
Publication Date
April 1, 1966
Subject Category
Fluid Mechanics
Report/Patent Number
WR-66-23
NASA-CR-76126
Report Number: WR-66-23
Report Number: NASA-CR-76126
Accession Number
66N30316
Funding Number(s)
CONTRACT_GRANT: NAS8-11308
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLOW VISUALIZATION
FLARED BODY
SUPERSONIC FLOW
SHADOWGRAPH
TURBULENT FLOW

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