Vibration of Laminated Composite Shells with Cutouts and Concentrated Mass
Author:
Affiliation:
1. NIT Patna, Patna 800 005, India
2. IIT Roorkee, Roorkee 247 667, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056320
Reference43 articles.
1. Dynamic response of composite plates with cut-outs, part I: Simply-supported plates
2. Strength Predictions of Composite Laminates with Unloaded Fastener Holes
3. Large amplitude flexural vibration of layered composite plates with cutouts
4. Vibration Of Plates With Cut-Outs Using Boundary Characteristic Orthogonal Polynomial Functions In The Rayleigh-ritz Method
5. Vibration of perforated doubly-curved shallow shells with rounded corners
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