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Supersonic flow around circular cones at angles of attackThe properties of conical flow without axial symmetry are analyzed. The flow around cones of circular cross section at small angles of attack is determined by correctly considering the effect of the entropy gradients in the flow.
Document ID
19930090960
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ferri, Antonio
Date Acquired
September 6, 2013
Publication Date
January 1, 1951
Report/Patent Number
NACA-TR-1045
Accession Number
93R20250
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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