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The Effect of a Simulated Propeller Slipstream on the Aerodynamic Characteristics of an Unswept Wing Panel with and Without Nacelles at Mach Numbers from 0.30 to 0.86
Document ID
19930083569
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Cole, Richard I
Jordan, Gareth H
Date Acquired
August 16, 2013
Publication Date
September 1, 1952
Report/Patent Number
NACA-TN-2776
Report Number: NACA-TN-2776
Accession Number
93R12859
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING - NACELLE COMBINATIONS - AIRPLANES
MACH NUMBER EFFECTS - WING SECTIONS
SLIPSTREAM - PROPELLERS

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