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Analytical study of effects of product of inertia on airplane spin entries, developed spins, and spin recoveriesInertia product and inertia moment variation effect on spin entry, developed spin, and spin recovery of airplanes
Document ID
19650011396
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Anglin, E. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-2754
Accession Number
65N20997
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRCRAFT
SPIN DYNAMICS
INERTIA MOMENT

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