Influence of Large Amplitudes on Flexural Vibrations of a Thin, Cylindrical, Sandwich Shell-Reference-Cited by-同舟云学术

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Influence of Large Amplitudes on Flexural Vibrations of a Thin, Cylindrical, Sandwich Shell

Published:1962-03 Issue:3 Volume:29 Page:376-376
ISSN:1936-9999
Container-title:Journal of the Aerospace Sciences
language:en
Short-container-title:Journal of the Aerospace Sciences

Author:

Chu Hugh N.¹

Affiliation:

1. The Martin Company, Denver, Colo.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.9461

Reference5 articles.

1. Tables of Supersonic Flow Around Cones, Tech. Rep. No. 1, M.I.T , 1947; Tables of Supersonic Flow Around Yawing Cones, Tech. Rep. No. 3, M.I.T., 1947; Tables of Supersonic Flow Around Cones of Large Yaw, Tech. Rep. No. 5, M.I.T.,1949.

2. Supersonic Flow at the Surface of a Circular Cone at Angle of Attack

3. Influence of Large Amplitudes on Flexural Vibrations of a Thin Circular Cylindrical Shell

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. On the mathematical models of the Timoshenko-type multi-layer flexible orthotropic shells;Nonlinear Dynamics;2018-03-14

2. Nonlinear oscillations of a three-layer and multi-layer plates and shells during periodic impacts (survey);Izvestiya MGTU MAMI;2014-07-10

3. Dynamics of composite, sandwich, and stiffened shell-type structures;Journal of Spacecraft and Rockets;1969-12

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