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机译:广义Weissinger的L方法用于预测在亚音速流中的自由表面上方运行的弯曲机翼
School of Naval Architecture Engineering, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, People's Republic of China;
School of Naval Architecture Engineering, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, People's Republic of China;
School of Naval Architecture Engineering, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, People's Republic of China;
School of Naval Architecture Engineering, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, People's Republic of China,School of Aeronautics and Astronautics, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, People's Republic of China Department of Mathematics, Imperial College London, London SW7 2AZ, UK;
School of Naval Architecture Engineering, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, People's Republic of China;
School of Naval Architecture Engineering, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, People's Republic of China;
School of Naval Architecture Engineering, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, People's Republic of China;
Curved wing; Free surface; Green's function; Stratified fluid; Weissinger's L-method; WIG effect;
机译:弯曲表面流体动力流动歧管的网状方法:广义移动最小二乘(GMLS)方法
机译:一种自由边界问题和普通声波曲线的退化椭圆方程和亚音速流动
机译:普朗特半经验理论在预测曲面上流动的传热和摩擦中的应用
机译:对Weissinger涡流装置的修改,以预测低纵横比机翼的侧滑所引起的稳定性导数
机译:具有通用基函数的自由形状曲线和曲面的直接形状控制。
机译:亚音速气流中机翼模型的颤振模式
机译:在高亚源热导热的自由表面运动上