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The experimental determination of the moments of inertia of airplanesThe application of the pendulum method to the experimental determination of the moments of inertia of airplanes is discussed in this report. Particular reference is made to the effects of the air, in which the airplane is immersed, on the swinging tests and to the procedure by which these effects are taken into account. This procedure has been used for some time, and the data on several airplanes for which the moments of inertia have been found are included.
Document ID
19930091541
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Soule, Hartley A
Miller, Marvel P
Date Acquired
September 6, 2013
Publication Date
January 1, 1934
Report/Patent Number
NACA-TR-467
Accession Number
93R20831
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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