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The Aerodynamic Forces and Moments on a 1/10-scale Model of a Fighter Airplane in Spinning Attitudes as Measured on a Rotary Balance in the Langley 20-foot Free-spinning Tunnel
Document ID
19930082832
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Stone, Ralph W , Jr
Burk, Sanger M , Jr
Bihrle, William, Jr
Date Acquired
August 16, 2013
Publication Date
September 1, 1950
Report/Patent Number
NACA-TN-2181
Report Number: NACA-TN-2181
Accession Number
93R12122
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
RUDDER CONTROLS
SPINNING - RECOVERY
ROLLING, PITCHING & YAWING MOMENTS
SPINNING TESTS, WIND-TUNNEL
MANEUVERABILITY - FIGHTERS
WIND TUNNEL TESTS - NACA - FREE-SPINNING (20 FEET)
SPINNING CHARACTERISTICS - EFFECT OF LANDING GEARS
SPINNING CHARACTERISTICS - EFFECT OF TAIL SURFACES
SPINNING CHARACTERISTICS - EFFECT OF WING FLAPS

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