机译:微型纤细导轨考虑空气弹性和辅助载荷的多学科设计优化
Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Minist Educ Key Lab Dynam & Control Flight Vehicle Beijing 100081 Peoples R China;
Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Minist Educ Key Lab Dynam & Control Flight Vehicle Beijing 100081 Peoples R China;
Tsinghua Univ Sch Aerosp Engn Beijing 100084 Peoples R China;
Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Minist Educ Key Lab Dynam & Control Flight Vehicle Beijing 100081 Peoples R China;
Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Minist Educ Key Lab Dynam & Control Flight Vehicle Beijing 100081 Peoples R China;
Long-range slender guided rockets; Multidisciplinary design optimization; Aeroelasticity; Subsidiary loads; Disciplinary modeling; Metamodel-based design optimization;
机译:考虑空气弹性和辅助载荷的远程细长型制导火箭弹的多学科设计优化
机译:远程导向火箭的空气动力学形状的多目标优化
机译:细长翼梁减少方法的基于梯度的气动弹性优化设计
机译:多学科机体设计过程:纳入稳定和非稳定的气动弹性载荷
机译:具有气动和气动弹性约束的飞机机翼结构的多学科设计优化。
机译:多学科设计优化问题中的交互预测优化
机译:期考虑辅助荷载作用的气弹远程火箭轨迹分析