倾转旋翼/机翼连续过渡状态气动性能仿真分析
王孟恬,金台,刘尧龙

Numerical analysis of tiltrotor/wing aerodynamic characteristics in continuous conversion mode
Mengtian WANG,Tai JIN,Yaolong LIU
图 10 旋翼与机翼之间的流场压力云图(J=0.2, α=90°)
Fig.10 Pressure contour of flow field between rotor and wing (J=0.2, α=90°)