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With the goal of improving flight performance across the entire flight regime, a modal based wing shaping optimization is carried out, subject to the requirement of trim and control cost limitation.
Based on the normalized integral square error index of inter-area rotor angle difference and specified structured H∞ loop shaping optimization, the robust SMES controller with the smallest coil size, can be achieved by the genetic algorithm.
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The first chapter is related to shape optimization of highly nonlinear coupled models.
This article is devoted to shape optimization design of pure bending beams under single loading condition.
The parts connected to shape optimization are described in more detail.
This paper is devoted to shape optimization of constrained contact force problem.
It can be confirmed that local optimal solutions exist in this shape optimization problem.
In this paper, we consider optimal design problems that involve shape optimization.
Therefore, shape optimization is needed to improve the hysteretic performance of the U-shaped damper.
The optimal design utilizes FEM software and MATLAB interactively to perform effective shape optimization.
Another optimization is curved wall shape optimization.
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