Dynamic response of two-layered cylindrical shells to time-dependent loads
Author:
Affiliation:
1. Lockheed Missiles and Space Company, Palo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference14 articles.
1. Flexural vibrations of the walls of thin cylindrical shells having freely supported ends
2. Tables for Frequencies and Modes of Free Vibration of Infinitely Long Thin Cylindrical Shells
3. Free Vibrations of Thin Cylindrical Shells Having Finite Lengths With Freely Supported and Clamped Edges
4. Vibrations of Thin Cylindrical Shells Analyzed by Means of Donnell-Type Equations
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1. Elasto/Visco-Plastic Dynamic Response of General Thin Shells to Blast Loads;Bulletin of JSME;1982
2. Forced Motions of Elastic Cylindrical Shells;Journal of Applied Mechanics;1975-06-01
3. Numerical Analysis of Dynamic Response of Axisymmetrical Shells to Time-Dependent Loads;Bulletin of JSME;1975
4. Composite Material Mechanics: Structural Mechanics;AIAA Journal;1974-09
5. An analysis of forced axisymmetric motions of Timoshenko-type cylindrical shells;Journal of Sound and Vibration;1973-10
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