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The experimental determination of the moments of inertia of airplanes by a simplified compound-pendulum methodA simplified compound-pendulum method for the experimental determination of the moments of inertia of airplanes about the x and y axes is described. The method is developed as a modification of the standard pendulum method reported previously in NACA report, NACA-467. A brief review of the older method is included to form a basis for discussion of the simplified method. (author)
Document ID
19930082299
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gracey, William
Date Acquired
August 16, 2013
Publication Date
June 1, 1948
Report/Patent Number
NACA-TN-1629
Accession Number
93R11589
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MOMENTS OF INERTIA
PENDULUM APPARATUS - NACA

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