滑流边界 meaning in Chinese

slip-flow boundary

The effects of the slipstream boundary are solved by the slipstream boundary condition met using the so - called vortex image method . based on these considerations , the change in the circulation around the wing is obtained , and the velocities induced by the original vortices and the imaged vortices at the wing are subsequently derived . the present research also gives an analytical expression of the drag change due to the slipstream interference
对于滑流边界的影响,用“镜像法”来使滑流边界条件得到满足,导出了由于滑流影响机翼环量的改变,求得涡及其镜像在机翼处的诱导,并首次导出了螺旋桨滑流对机翼阻力特性的影响的解析表达式。