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TECHNICAL PAPERS

Stability of the Shanley Column Under Cyclic Loading

[+] Author and Article Information
E. Corona

Department of Aerospace and Mechanical Engineering, University of Notre Dame, Notre Dame, IN 46556

J. Appl. Mech 68(2), 324-331 (Jun 28, 2000) (8 pages) doi:10.1115/1.1349118 History: Received March 20, 2000; Revised June 28, 2000
Copyright © 2001 by ASME
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References

Figures

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Plasticity model parameters
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Response history under load control for a model with L/b=150 for different load amplitudes, (a) peak values of vertical displacement in each cycle as function of cycle number, (b) peak values of θ in each cycle as function of cycle number
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Response history in terms of peak θ values as function of cycle number under load control for different values of initial imperfection, (a) L/b=50, (b) L/b=100
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Monotonic response, (a) load-axial deflection response of three models, (b) corresponding load-rotation response
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Cyclic response under symmetric displacement control for a model with L/b=50, (a) load-axial deflection response, (b) corresponding load-rotation response
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Stress-strain response for the case in Fig. 4, (a) link 1, (b) link 2
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Peak values of θ in each cycle as a function of cycle number for various cycle amplitudes under displacement control
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Cyclic response under symmetric displacement control for a model with L/b=100, (a) load-axial deflection response, (b) corresponding load-rotation response
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Stress-strain histories for the first cycle of the response shown in Fig. 7
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Cyclic response under symmetric load control for a model with L/b=50, (a) load-axial deflection response, (b) corresponding load-rotation response
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Stress-strain response under symmetric load control for the case in Fig. 9, (a) link 1, (b) link 2
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Response history under load control for a model with L/b=50 for different load amplitudes, (a) peak values of vertical displacement in each cycle as function of cycle number, (b) peak values of θ in each cycle as function of cycle number
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Response history under load control for a model with L/b=100 for different load amplitudes, (a) peak values of vertical displacement in each cycle as function of cycle number, (b) peak values of θ in each cycle as function of cycle number
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Response in terms of peak values of u and θ in each half-cycle for a model with L/b=100 and Ñ/|Ncr|=0.70 under load control
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(a) Shanley column, (b) deflected configuration and free-body diagram

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