机译:不同传入流动速度的前缘板块内部自激振荡强度调查
Beihang Univ Minist Ind & Informat Technol Key Lab Aeroacoust Beijing 100191 Peoples R China|Beihang Univ Minist Educ Key Lab Fluid Mech Beijing 100191 Peoples R China|Beihang Univ Sch Aeronaut Sci & Engn Beijing 100191 Peoples R China;
Beihang Univ Minist Ind & Informat Technol Key Lab Aeroacoust Beijing 100191 Peoples R China|Beihang Univ Minist Educ Key Lab Fluid Mech Beijing 100191 Peoples R China|Beihang Univ Sch Aeronaut Sci & Engn Beijing 100191 Peoples R China;
Beihang Univ Minist Ind & Informat Technol Key Lab Aeroacoust Beijing 100191 Peoples R China|Beihang Univ Minist Educ Key Lab Fluid Mech Beijing 100191 Peoples R China|Beihang Univ Sch Aeronaut Sci & Engn Beijing 100191 Peoples R China;
Beihang Univ Minist Ind & Informat Technol Key Lab Aeroacoust Beijing 100191 Peoples R China|Beihang Univ Minist Educ Key Lab Fluid Mech Beijing 100191 Peoples R China|Beihang Univ Sch Aeronaut Sci & Engn Beijing 100191 Peoples R China;
Leading-edge slat; Aerodynamic noise characteristics; Incoming flow speed; Tones; Intensity;
机译:在不同输入流速下前沿板条湾内自激振荡引起的音调强度研究
机译:在不同攻击角度下引导边板湾自我激发振荡的调查:频率和强度
机译:可变弯曲板块对大小的自我激发振荡而对音调的影响
机译:板条湾中非定常流动和噪声源的研究:混合区域RANS / LES模拟和专用实验
机译:自激叶尖流动不稳定性和叶片行相互作用对低速和跨音速压缩机转子性能预测影响的数值研究。
机译:自激振荡脉冲水射流喷丸处理表面质量的实验研究
机译:在流动音的产生过程中通过腔的自激振荡的成像
机译:在流动音的产生过程中通过腔的自激振荡的成像