全部

1·With this new shape, the vertical gurney flap (2) has been reduced.

与新的改动相配套，垂直gurney襟翼(2)缩小了。

2·The effects of Gurney flap on double delta wing aerodynamic performance in low speed wind-tunnel tests;

双三角翼气动布局比三角翼飞机具有更好的大攻角空气动力特性。

3·Force and PIV local flow measurements were conducted in a low speed wind tunnel to study the effectiveness of serrated Gurney flap at different deflections.

用低速风洞测力试验和襟翼处绕流的PIV测量试验研究锯齿形格尼襟翼在不同偏角下的增升效益。