A theory for the free vibration of a laminated composite rectangular plate with holes in aerospace applications

Author:

Kim Yongha,Park Jungsun

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference22 articles.

1. Surrogate-based optimization with improved support vector regression for non-circular vent hole on aero-engine turbine disk;Cheng;Aerosp Sci Technol,2020

2. Equivalent and simplification of nickel-based single crystal plates with film cooling holes;Zhixun;Aerosp Sci Technol,2018

3. Geometrically nonlinear static aeroelastic analysis of composite morphing wing with corrugated structures;Natsuki;Aerosp Sci Technol,2019

4. Low energy actuation technique of bistable composites for aircraft morphing;Nicassio;Aerosp Sci Technol,2018

5. Free vibration of laminated composite plates with a central circular hole;Chai;Compos Struct,1996

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