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 15 V=67 m/s典型工况纵向气动力试验结果(不同转捩位置)
Fig.15 Experiment results of longitudinal aerodynamic force under typical inflow conditions when V=67 m/s (different transition positions)