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Optimization of Nonlinear Lateral Characteristic of Lifting-Body Type Reentry Vehicle

机译:升降式再入飞行器非线性侧向特性的优化

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摘要

The nonlinear lateral characteristics of a lifting-body type reentry vehicle were improved by applying efficient optimization techniques to determine the optimum configuration. First, the causes for the nonlinear lateral characteristics were investigated by computational fluid dynamics analysis. The results indicated that fins mounted on the Japan Aerospace Exploration Agency's baseline lifting-body configuration cause unsymmetrical development of vortices and result in nonlinear lateral characteristics. An efficient optimization algorithm, called efficient global optimization for multiobjective problems, was adopted to improve these nonlinear lateral characteristics. Efficient global optimization for multiobjective problems predicts potential optimum solutions based on the probability estimated by the Kriging model. The computational time for optimization was markedly reduced owing to use of the Kriging model. Further investigations were also performed to determine the effects of the upswept upper-aft and swept-back fin angles. The results indicated that the swept-back fin angle is an important factor controlling the lateral characteristics of the lifting-body type reentry vehicle.
机译:通过应用有效的优化技术来确定最佳配置,可以改善举升式折返车的非线性横向特性。首先,通过计算流体动力学分析研究了非线性横向特性的原因。结果表明,安装在日本航空航天局基本举升体构型上的鳍片会导致涡旋不对称发展,并导致非线性的侧向特性。采用了一种有效的优化算法,称为多目标问题的有效全局优化,以改善这些非线性横向特性。针对多目标问题的有效全局优化基于Kriging模型估计的概率来预测潜在的最佳解决方案。由于使用了克里格模型,优化的计算时间大大减少了。还进行了进一步的研究,以确定上扫后尾鳍和后扫尾鳍角度的影响。结果表明,后掠鳍角是控制举升式再入车辆横向特性的重要因素。

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