Vibration Induced Fatigue Analysis of [0n/90n]s Simply Supported Composite Plate Under Central Patch Impulse Loading
Author:
Affiliation:
1. Aerospace Engineering Department, Indian Institute of Technology Bombay, Powai, Mumbai 400076, India e-mail:
2. Civil Engineering Department, Indian Institute of Technology Bombay, Powai, Mumbai 400076, India e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science
Link
http://asmedigitalcollection.asme.org/materialstechnology/article-pdf/doi/10.1115/1.4030338/6135301/mats_137_04_044501.pdf
Reference56 articles.
1. Fatigue Behavior of [0n/90n]s Composite Cantilever Beam Under Tip Impulse Loading;Compos. Struct.,2013
2. Random Response of Symmetric Cross-Ply Composite Beams With Arbitrary Boundary Conditions;AIAA J.,1992
3. Dynamic Finite Element Analysis of Laminated Beam With Delamination Cracks Using Contact Impact Conditions;Compos. Struct.,1996
4. Finite Element Dynamic Analysis of Unsymmetric Composite Laminated Beams With Shear Effect and Rotary Inertia Under the Action of Moving Loads;Finite Elem. Anal. Design,1998
5. Stochastic Vibration of Laminated Composite Coated Beam Traversed by a Random Moving Load;Eng. Struct.,2003
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