一种高升阻比非常规翼身融合燕尾气动布局
刘柳, 向先宏, 张宇飞, 陈海昕, 魏闯, 朱剑, 杨普

A high lift-to-drag ratio unconventional blended-wing-body aerodynamic configuration with swallow tail
Liu LIU, Xianhong XIANG, Yufei ZHANG, Haixin CHEN, Chuang WEI, Jian ZHU, Pu YANG
图 21 V=67 m/s时不同迎角下机翼表面流线计算和丝线试验对比结果
Fig.21 Comparison of calculated surface streamlines and silk test results of wing at different angles of attack when V=67 m/s