An optimization strategy is proposed to deal with the aerodynamic/stealthy/structural multidisciplinary design optimization （MDO） issue of unmanned combat air vehicle （UCAV）. In applying the strategy, the MDO proc...An optimization strategy is proposed to deal with the aerodynamic/stealthy/structural multidisciplinary design optimization （MDO） issue of unmanned combat air vehicle （UCAV）. In applying the strategy, the MDO process is divided into two levels, i.e. system level optimization and subsystem level optimization. The system level optimization is to achieve optimized system objective （or multi-objective） through the adjustment of global external configuration design variables. The subsystem level optimization consists of the aerodynamic/stealthy integrated design and the structural optimization. The aerodynamic/stealthy integrated design aims at achieving the minimum aerodynamic drag coefficient under the constraint of stealthy requirement through the adjustment of local external configuration design variables. The structural optimization is to minimize the structural weight by adjusting the dimefisions of structural components. A flowchart to implement this strategy is presented. The MDO for a flying-wing configuration of UCAV is employed to illustrate the detailed process of the optimization. The results indicate that the overall process of the surrogate-based two-level optimization strategy can be implemented automatically, and quite reasonable results are obtained.展开更多
提出了疲劳寿命预腐蚀影响系数曲线(C- T 曲线)通用性分析的 C值直接对比法和C -T 曲线参数统计对比法,并进行相关试验研究,得到了 C -T 曲线和载荷谱、应力水平以及裂纹尺寸基本无关的结论。C- T曲线是进行腐蚀条件下飞机结构疲劳寿命...提出了疲劳寿命预腐蚀影响系数曲线(C- T 曲线)通用性分析的 C值直接对比法和C -T 曲线参数统计对比法,并进行相关试验研究,得到了 C -T 曲线和载荷谱、应力水平以及裂纹尺寸基本无关的结论。C- T曲线是进行腐蚀条件下飞机结构疲劳寿命评定和分析的基础,为验证分析 C- T 曲线和载荷谱、应力水平以及裂纹尺寸的相关性,从C的定义和分布规律出发,提出了 C值直接对比法和C -T 曲线参数统计对比法,近似谱、不同恒幅应力水平以及不同指定裂纹尺寸下的预腐蚀疲劳寿命数据均表明了 C- T 曲线基本具有通用性;并进行了某型飞机结构主梁模拟试件在随机谱及恒幅谱下的预腐蚀疲劳试验,试验结果同样验证了上述结论,从而说明了C- T 曲线的通用性。展开更多
文摘An optimization strategy is proposed to deal with the aerodynamic/stealthy/structural multidisciplinary design optimization （MDO） issue of unmanned combat air vehicle （UCAV）. In applying the strategy, the MDO process is divided into two levels, i.e. system level optimization and subsystem level optimization. The system level optimization is to achieve optimized system objective （or multi-objective） through the adjustment of global external configuration design variables. The subsystem level optimization consists of the aerodynamic/stealthy integrated design and the structural optimization. The aerodynamic/stealthy integrated design aims at achieving the minimum aerodynamic drag coefficient under the constraint of stealthy requirement through the adjustment of local external configuration design variables. The structural optimization is to minimize the structural weight by adjusting the dimefisions of structural components. A flowchart to implement this strategy is presented. The MDO for a flying-wing configuration of UCAV is employed to illustrate the detailed process of the optimization. The results indicate that the overall process of the surrogate-based two-level optimization strategy can be implemented automatically, and quite reasonable results are obtained.
文摘提出了疲劳寿命预腐蚀影响系数曲线(C- T 曲线)通用性分析的 C值直接对比法和C -T 曲线参数统计对比法,并进行相关试验研究,得到了 C -T 曲线和载荷谱、应力水平以及裂纹尺寸基本无关的结论。C- T曲线是进行腐蚀条件下飞机结构疲劳寿命评定和分析的基础,为验证分析 C- T 曲线和载荷谱、应力水平以及裂纹尺寸的相关性,从C的定义和分布规律出发,提出了 C值直接对比法和C -T 曲线参数统计对比法,近似谱、不同恒幅应力水平以及不同指定裂纹尺寸下的预腐蚀疲劳寿命数据均表明了 C- T 曲线基本具有通用性;并进行了某型飞机结构主梁模拟试件在随机谱及恒幅谱下的预腐蚀疲劳试验,试验结果同样验证了上述结论,从而说明了C- T 曲线的通用性。
