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Analysis of Wind-tunnel Tests to a Mach Number of 0.90 of a Four-engine Propeller-driven Airplane Configuration Having a Wing with 40 Degrees of Sweepback and an Aspect Ratio of 10
Document ID
19930084498
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Edwards, George G
Buell, Donald A
Demele, Fred A
Sutton, Fred B
Date Acquired
August 16, 2013
Publication Date
September 1, 1956
Report/Patent Number
NACA-TN-3790
Accession Number
93R13788
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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