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Spin-tunnel investigation of the effects of mass and dimensional variations on the spinning characteristics of a low-wing single-vertical-tail model typical of personal-owner airplanes
Document ID
19930083028
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Klinar, Walter J
Wilson, Jack H
Date Acquired
August 29, 2013
Publication Date
May 1, 1951
Report/Patent Number
NACA-TN-2352
Report Number: NACA-TN-2352
Accession Number
93R12318
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRPLANES - MODELS - MASS DISTRIBUTION
SPINNING - RECOVERY
SPINNING CHARACTERISTICS - EFFECT OF WING-TAIL COMBINATIONS
WIND TUNNEL TESTS - NACA - FREE-SPINNING (20 FEET)
SPINNING TESTS - AIRPLANES, LIGHT

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