It is well known that the in-plane stress and displacement distributions in a stationary annular disk under stationary edge tractions can be obtained through the use of Airy stress function in the classical theory of linear elasticity. By using Lame’s potentials, this paper extends these solutions to the case of a spinning disk under stationary edge tractions. It is also demonstrated that the problem of stationary disk-spinning load differs from the problem of spinning disk-stationary load not only by the centrifugal effect, but also by additional terms arising from the Coriolis effect. Numerical simulations show that the amplitudes of the stress and displacement fields grow unboundedly as the rotational speed of the disk approaches the critical speeds. As the rotational speed approaches zero, on the other hand, the in-plane stresses and displacements are shown, both numerically and analytically, to recover the classical solutions derived through the Airy stress function.
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December 1997
Technical Papers
In-Plane Stress and Displacement Distributions in a Spinning Annular Disk Under Stationary Edge Loads
Jen-San Chen,
Jen-San Chen
Department of Mechanical Engineering, National Taiwan University, Taipei, Taiwan 107, Republic of China
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Jhi-Lu Jhu
Jhi-Lu Jhu
Department of Mechanical Engineering, National Taiwan University, Taipei, Taiwan 107, Republic of China
Search for other works by this author on:
Jen-San Chen
Department of Mechanical Engineering, National Taiwan University, Taipei, Taiwan 107, Republic of China
Jhi-Lu Jhu
Department of Mechanical Engineering, National Taiwan University, Taipei, Taiwan 107, Republic of China
J. Appl. Mech. Dec 1997, 64(4): 897-904 (8 pages)
Published Online: December 1, 1997
Article history
Received:
June 26, 1995
Revised:
May 22, 1997
Online:
October 25, 2007
Citation
Chen, J., and Jhu, J. (December 1, 1997). "In-Plane Stress and Displacement Distributions in a Spinning Annular Disk Under Stationary Edge Loads." ASME. J. Appl. Mech. December 1997; 64(4): 897–904. https://doi.org/10.1115/1.2788997
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