Finite element analysis of vibrations of initially stressed thin shells of revolution-Reference-Cited by-同舟云学术

Finite element analysis of vibrations of initially stressed thin shells of revolution

Published:1974-11 Issue:1 Volume:37 Page:57-64
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Venkateswara Rao G.,Sundararamaiah V.,Raju I.S.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference8 articles.

1. A method for computation of vibration modes and frequencies of orthotropic thin shells of revolution having general meridional curvature;Adelman;NASA TN D-4972,1969

2. A reinvestigation of buckling of shells of revolution by a refined finite element;Venkateswara Rao;American Institute of Aeronautics and Astronautics Journal,1974

3. Non-linear theories of thin shells;Sanders;Quarterly of Applied Mathematics,1963

4. Stability analysis of shells of revolution by the finite element method;Navaratna;American Institute of Aeronautics and Astronautics Journal,1968

5. K. Singa Rao, N. Muthiyalu and C. L. Amba-Rao (To be published.) A reappraisal of vibration, in-plane load relationship of elastically restrained circular plates.

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