Free Vibration of Thick Generally Laminated Quadrilateral Plates Having Arbitrarily Located Point Supports

Author:

Kapania Rakesh K.1,Lovejoy Andrew E.1

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061-0203

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 6 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. Vibration of Curvilinearly Stiffened Plates Using Ritz Method With Orthogonal Jacobi Polynomials;Journal of Vibration and Acoustics;2019-11-18

2. Integrated Local Petrov-Galerkin Sinc Method for Structural Mechanics Problems;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04

3. Modelling Continuously Morphing Aircraft for Flight Control;AIAA Guidance, Navigation and Control Conference and Exhibit;2008-06-15

4. Features of the flexural vibrations of plates with a locally fixed boundary contour;International Applied Mechanics;2002

5. Static and Vibration Analyses of General Wing Structures Using Equivalent-Plate Models;AIAA Journal;2000-07

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