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Viscous effects on the flow coefficient for a supersonic nozzle
Adiabatic flow coefficient in supersonic nozzle with choked flow conducted over throat Reynolds number range
Document ID
19700049883
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Back, L. H.
Massier, P. F.
Noel, M. B.
Saheli, F.
Date Acquired
August 5, 2013
Publication Date
March 1, 1970
Subject Category
Aerodynamics
Accession Number
70A25999
Distribution Limits
Public
Copyright
Other
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