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机译:加强飞机尾翼前缘结构以防鸟击的新颖设计
Northwestern Polytech Univ, Sch Aeronaut, Xian 710072, Peoples R China;
Northwestern Polytech Univ, Sch Aeronaut, Xian 710072, Peoples R China;
Northwestern Polytech Univ, Sch Aeronaut, Xian 710072, Peoples R China;
Northwestern Polytech Univ, Sch Aeronaut, Xian 710072, Peoples R China;
Univ Akron, Dept Mech Engn, Akron, OH 44325 USA;
Commercial Aircraft Corp China Ltd, Shanghai 200120, Peoples R China;
Commercial Aircraft Corp China Ltd, Shanghai 200120, Peoples R China;
Bird strike; Design; Experiment; Simulation; Tail leading edge;
机译:垂直尾翼前缘结构连接设计中抗鸟击性能的数值分析
机译:由金属纤维层压板制成的飞机机翼前缘上的鸟击的建模-第2部分:SPH鸟模型的冲击建模
机译:鸟击对三明治复合飞机翼前缘的影响
机译:新型动态失效模型对飞机前缘结构鸟击的数值模拟
机译:设计和制造两架带有先进旋转前缘机翼的飞机。
机译:鱼尾运动形成一个附着的前缘涡旋
机译:复合材料抗鸟撞前缘的设计和测试