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M. Ganapathi

Researcher at VIT University

Publications -  102
Citations -  3684

M. Ganapathi is an academic researcher from VIT University. The author has contributed to research in topics: Finite element method & Rotary inertia. The author has an hindex of 33, co-authored 102 publications receiving 3142 citations. Previous affiliations of M. Ganapathi include Indian Institute of Technology Madras & Indian Institute of Technology Delhi.

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Assessment of certain higher-order structural models based on global approach for bending analysis of curvilinear composite laminates

Anand Venkatachari, +3 more
- 01 Dec 2014 - 
TL;DR: In this article, the performance of different structural models based on global approach in evaluating the static response of curvilinear fiber composite laminates is analyzed, and a C o shear flexible Quad-8 element developed based on higher-order structural theory is employed for the present study.
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Supersonic Flutter of Laminated Curved Panels

M. Ganapathi, +1 more
- 01 Jan 1995 - 
TL;DR: In this article, the aerodynamic force of laminated composite curved panels is evaluated using two-dimensional static aerodynamic approximation for high supersonic flow using doubly-curved, quadrilateral, shear flexible, shell element based on field consistency approach.
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Supersonic flutter study of porous 2D curved panels reinforced with graphene platelets using an accurate shear deformable finite element procedure

S. Aditya, +4 more
- 01 Jun 2020 - 
TL;DR: In this article, the authors investigated the flutter behavior of two-dimensional porous curved panels reinforced by graphene platelets exposed to supersonic flow on one side of the panels using the trigonometric shear deformation theory.
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Buckling characteristics of cross-ply elliptical cylinders under axial compression

C. T. Sambandam, +4 more
- 01 Oct 2003 - 
TL;DR: In this article, the elastic buckling characteristics of laminated cross-ply elliptical cylindrical shells under axial compression was studied through finite element approach, and the governing equations obtained using the principle of minimum potential energy were solved through eigenvalue approach.
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Application of a field-consistent shear flexible element for nonlinear dynamic analysis of laminated shells

M. Ganapathi, +1 more
- 01 Oct 1992 - 
TL;DR: In this article, a doubly curved laminated, C 0 shear flexible quad -8 shell element based on the field consistency principle was used to investigate the nonlinear transient response of anisotropic laminated plates/shells.