机译:分布式粗糙度元素对Naca0012翼型边界层过渡的影响
Nanjing Univ Aeronaut &
Astronaut Coll Aerosp Engn Nanjing Jiangsu Peoples R China;
Nanjing Univ Aeronaut &
Astronaut Coll Aerosp Engn Nanjing Jiangsu Peoples R China;
Nanjing Univ Aeronaut &
Astronaut Coll Aerosp Engn Nanjing Jiangsu Peoples R China;
Nanjing Univ Aeronaut &
Astronaut Coll Aerosp Engn Nanjing Jiangsu Peoples R China;
Nanjing Univ Aeronaut &
Astronaut Coll Aerosp Engn Nanjing Jiangsu Peoples R China;
Oil-film interferometry; distributed roughness elements; skin friction; boundary layer transition; airfoil;
机译:分布式粗糙度元素对Naca0012翼型边界层过渡的影响
机译:三维边界层过渡的被动控制,重点是离散的粗糙度元素
机译:锯齿形壁对NACA0012机翼冲击波/边界层相互作用的被动控制数值评估
机译:高升降机翼型压力梯度下表面粗糙度对平板边界层过渡的影响及低自由流湍流
机译:翼型前缘附近较大的分布粗糙度对边界层发展和过渡的影响。
机译:前沿充气风筝翼型的边界层过渡建模
机译:前缘粗糙度对振荡翼型边界层过渡的影响