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Measurement of the Moment of Inertia of Missile‐type Bodies: A Modified Bifilar Torsion Pendulum Formula

A.B. Schwartz (Project Weight Engineer, Initial Projects Office, Avro Aircraft Ltd.)
S. Malick (Project Weight Estimator, Initial Projects Office, Avro Aircraft Ltd.)
J.R. Friesen (Project Weight Estimator, Initial Projects Office, Avro Aircraft Ltd.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 September 1957

187

Abstract

THE experimental determination of the moment of inertia of a body is frequently required to confirm a calculated value or to eliminate the tedious work involved in the calculation. This is normally done by integrating the body into a vibrating system, such as a pendulum.

Citation

Schwartz, A.B., Malick, S. and Friesen, J.R. (1957), "Measurement of the Moment of Inertia of Missile‐type Bodies: A Modified Bifilar Torsion Pendulum Formula", Aircraft Engineering and Aerospace Technology, Vol. 29 No. 9, pp. 271-274. https://doi.org/10.1108/eb032869

Publisher

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MCB UP Ltd

Copyright © 1957, MCB UP Limited

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