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Full Scale Drag Tests on Various Parts of Sperry Messenger AirplaneThe drag of a Sperry Messenger airplane with the wings removed, and also the drag of its various component parts, was measured in the 20-foot air stream of the N.A.C.A. propeller research tunnel at air speeds from 50 to 100 m.p.h. It was found that the three-cylinder radial air-cooled engine nearly doubled the drag of the bare fuselage, and the drag of the landing gear was about the same as that of the fuselage and engine combined.
Document ID
19930081033
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Weick, Fred E
Date Acquired
September 6, 2013
Publication Date
January 1, 1928
Report/Patent Number
NACA-TN-271
Accession Number
93R10323
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRPLANES - WIND TUNNEL TESTS DRAG TESTS - SPERRY MESSENGER
LANDING GEARS - DRAG WIND TUNNEL TESTS (NACA P R T )
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