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Experimental study of a method of designing the sweptback-wing-fuselage juncture to reduce the drag at moderate supersonic speeds
Document ID
19930089007
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Howell, Robert R
Date Acquired
August 29, 2013
Publication Date
January 10, 1956
Report/Patent Number
NACA-RM-L55H05a
Report Number: NACA-RM-L55H05a
Accession Number
93R18297
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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