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Conical shock-wave angle.Conical shock-wave angle expressions compared for axisymmetric air flow past cone with attached shock wave
Document ID
19650038033
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hord, R. A.
Date Acquired
August 2, 2013
Publication Date
July 1, 1964
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-RP-457
Report Number: NASA-RP-457
Accession Number
65A20737
Distribution Limits
Public
Copyright
Other
Keywords
SHOCK WAVE
AXISYMMETRIC FLOW
CONICAL FLOW

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