论文部分内容阅读
应用染色液流动显示技术研究了雷诺数对６０°尖前缘三角翼前缘涡破裂位置、背风面流动结构等的影响，并详细分析了背风面流动随攻角的变化．
The effect of Reynolds number on vortex rupture location and leeward flow structure of 60 ° leading edge delta front was studied by using liquid flow display technology. The variation of incident angle of attack on leeward side was analyzed in detail.