On the Use of Reduced-Order Models for a Shallow Curved Beam Under Combined Loading
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American Institute of Aeronautics and Astronautics
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1. A FINITE ELEMENT TIME DOMAIN MODAL FORMULATION FOR LARGE AMPLITUDE FREE VIBRATIONS OF BEAMS AND PLATES
2. A COMBINED MODAL/FINITE ELEMENT ANALYSIS TECHNIQUE FOR THE DYNAMIC RESPONSE OF A NON-LINEAR BEAM TO HARMONIC EXCITATION
3. Determination of nonlinear stiffness with application to random vibration of geometrically nonlinear structures
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