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机译:杆-机翼相互作用噪声波浪形前缘的数值研究
Northwestern Polytech Univ, Sch Power & Energy, Xian 710129, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sch Power & Energy, Xian 710129, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sch Power & Energy, Xian 710129, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sch Power & Energy, Xian 710129, Shaanxi, Peoples R China;
China Aerodynam Res & Dev Ctr, State Key Lab Aerodynam, Mianyang 621000, Sichuan, Peoples R China;
机译:采用多孔材料和锯齿的杆翼型配置领先边缘降噪的数值研究
机译:波纹领先边缘对杆 - 航空互动噪声的实验研究
机译:杆翼型构型通过前缘锯齿减轻空气动力噪声的数值分析
机译:波浪形前沿降低湍流与机翼相互作用的噪声:实验和数值研究
机译:尾翼相互作用噪声主动和被动控制前沿装置的理论研究
机译:固定翼和旋转翼型后缘噪声的实验研究
机译:采用多孔材料和锯齿的杆翼型配置上前缘降噪的数值研究