The control of the post-buckling response in thin composite plates using smart technology

Restoration forces, associated with embedded activated pre-strained shape m emory alloy wires, have successfully been employed to enhance the post-buck ling behaviour of various laminated plate structures. An extensive experime ntal and numerical programme has been conducted, the results of which will be presented. The manufacturing methodology of the hybrid SMA/carbon/epoxy plates is outlined. Such specimens feature 0.4-mm diameter shape memory all oy wires located within tubing at desired locations. Numerical thermal anal ysis has been employed to predict the non-uniform temperature profile, attr ibuted to shape memory alloy activation through resistive heating, within t he laminates. Structural finite element analysis has been employed to deter mine the hybrid plates' adaptive response while under the influence of a un iaxial compressive load in excess of its critical buckling value. It is sho wn that, utilising the considerable control authority generated, even for a small actuator volume fraction, the out-of-plane displacement of the post- buckled laminates can be significantly reduced. Such displacement alleviati on allows for load redistribution away from the specimens' unloaded edges. With the increase in use of composite materials within aerospace platforms, it is envisaged that the hybrid adaptive SMA/laminate configuration will e xtend the operational performance over conventional materials and structure s, particularly when the structure is exposed to an elevated temperature. ( C) 2000 Elsevier Science Ltd. All rights reserved.