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The influence of very heavy fuselage mass loadings and long nose lengths upon oscillations in the spin
Document ID
19930082194
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Stone, Ralph W , Jr
Klinar, Walter J
Date Acquired
August 29, 2013
Publication Date
January 1, 1948
Report/Patent Number
NACA-TN-1510
Report Number: NACA-TN-1510
Accession Number
93R11484
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRPLANES - MODELS - MASS DISTRIBUTION
OSCILLATIONS - INERTIA
SPINNING - RECOVERY
FUSELAGE NOSES, EXTENDED
ROLLING & YAWING MOMENTS
SPINNING CHARACTERISTICS
WIND TUNNEL TESTS - NACA - FREE-SPINNING (15')
FUSELAGES - MASS DISTRIBUTION
WIND TUNNEL TESTS - NACA - FREE-SPINNING (20')
MOMENTS OF INERTIA

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