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Investigation of a Supersonic-inlet - Turbojet-engine Combination at Mach 2.0 and Angles of Attack up to 6 Degrees
Document ID
19930089754
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hearth, Donald P
Musial, Norman T
Date Acquired
August 16, 2013
Publication Date
July 1, 1957
Report/Patent Number
NACA-RM-E57D18
Report Number: NACA-RM-E57D18
Accession Number
93R19044
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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