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机译:桨距桨叶翼型非定常过渡的实验研究
Institute of Aerodynamics and Flow Technology, German Aerospace Center (DLR), Gottingen, Germany;
Institute of Aerodynamics and Flow Technology, German Aerospace Center (DLR), Gottingen, Germany;
Institute of Aerodynamics and Flow Technology, German Aerospace Center (DLR), Gottingen, Germany;
Institute of Aeroelasticity German Aerospace Center (DLR)Gottingen, Germany;
Institute of Aerodynamics and Gas Dynamics University of Stuttgart Stuttgart, Germany;
Institute of Aerodynamics and Flow Technology German Aerospace Center (DLR) Braunschweig, Germany;
机译:轴流压气机转子叶片表面非定常压力的实验研究
机译:使用k-ω-γ过渡模型对俯仰翼型进行非稳态过渡研究
机译:雷诺数过渡的俯仰翼型三维涡结构的实验和数值研究
机译:桨叶叶片翼型非定常过渡的实验研究
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:半椭圆叶片垂直轴风力发电机H转子研究的实验数据
机译:轴流压气机转子叶片表面非定常压力的实验研究
机译:具有双圆弧翼型叶片截面的跨音速轴流压气机转子的实验研究III:叶片元件性能与三级坚固度的比较