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NASA NTRS ยท 19740020294

Rotation in vibration, optimization, and aeroelastic stability problems

Abstract

The effects of rotation in the areas of vibrations, dynamic stability, optimization, and aeroelasticity were studied. The governing equations of motion for the study of vibration and dynamic stability of a rapidly rotating deformable body were developed starting from the nonlinear theory of elasticity. Some common features such as the limitations of the classical theory of elasticity, the choice of axis system, the property of self-adjointness, the phenomenon of frequency splitting, shortcomings of stability methods as applied to gyroscopic systems, and the effect of internal and external damping on stability in gyroscopic systems are identified and discussed, and are then applied to three specific problems.

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BibTeXRIS

Kaza, K. R. V.. 1974-05-01. Rotation in vibration, optimization, and aeroelastic stability problems. https://ntrs.nasa.gov/citations/19740020294

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