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Effect of yaw and angle of attack pressure recovery and mass-flow characteristics of a rectangular supersonic scoop inlet at a Mach number of 2.71
Document ID
19930089381
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Comenzo, Raymond J
Mackley, Ernest A
Date Acquired
August 29, 2013
Publication Date
September 10, 1954
Report/Patent Number
NACA-RM-L54G22
Report Number: NACA-RM-L54G22
Accession Number
93R18671
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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