Zeroth-Order Shear Deformation Theory for Plates
Author:
Affiliation:
1. Indian Institute of Technology, Powai, Mumbai 400 076, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.750
Reference19 articles.
1. Dynamic stability of a flexible missile under constant and pulsating thrusts
2. Asymptotic solutions to a stability problem
3. Nonlinear dynamic buckling of a compressed elastic column
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