Numerical eigenfrequency and experimental verification of variable cutout (square/rectangular) borne layered glass/epoxy flat/curved panel structure-Reference-Cited by-同舟云学术

Numerical eigenfrequency and experimental verification of variable cutout (square/rectangular) borne layered glass/epoxy flat/curved panel structure

Published:2020-05-07 Issue: Volume: Page:1-18
ISSN:1539-7734
Container-title:Mechanics Based Design of Structures and Machines
language:en
Short-container-title:Mechanics Based Design of Structures and Machines

Author:

Dewangan Hukum Chand¹,Sharma Nitin²,Hirwani Chetan Kumar³,Panda Subrata Kumar¹

Affiliation:

1. Department of Mechanical Engineering, National Institute of Technology Rourkela, Rourkela, Odisha, India;

2. School of Mechanical Engineering, KIIT University, Bhubaneswar, Odisha, India;

3. Department of Mechanical Engineering, National Institute of Technology Patna, Patna, Bihar, India

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Condensed Matter Physics,Aerospace Engineering,Automotive Engineering,General Mathematics,Civil and Structural Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/15397734.2020.1759432

Reference40 articles.

1. Free vibration analysis of cantilever open-hole composite plates

2. Nonlinear vibration analysis of viscoelastic micro nano-composite sandwich plates integrated with sensor and actuator

3. Eigen-frequency analysis of spherical shell laminated composite plates with and without central cutouts using finite elements

4. Free vibration of laminated composite plates with a central circular hole

5. Vibration of laminated composite panels and curved plates with different types of FGM composite constituent

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