
In order to increase aerodynamic efficiency, it is desirable to change the shape of the contour of the wings of an airplane for different flight conditions. This for example can be achieved by a compliant structure, which can be deformed without joints. In this presentation, the mechanical structural optimization of such a compliant mechanism is presented.
lattice structure, superelasticity, functionally graded material, structural optimization, multiscale optimization
lattice structure, superelasticity, functionally graded material, structural optimization, multiscale optimization
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