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Supersonic-area-rule Design and Rocket-propelled Flight Investigation of a Zero-lift Straight-wing--body--nacelle Configuration Between Mach Numbers 0.8 and 1.53
Document ID
19930089180
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hoffman, Sherwood
Date Acquired
August 16, 2013
Publication Date
April 26, 1956
Report/Patent Number
NACA-RM-L56B27
Report Number: NACA-RM-L56B27
Accession Number
93R18470
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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