结果表明，该机翼的转捩位置在离开机翼前缘的70％左右的当地弦长处。
The results show that the transition position of the wing is at about 70% local chord from wing leading edge.
火焰面紧跟在激波前缘的后面，二者同速传播，超压峰值的位置与火焰面重合。
Flame front closely follows Shockwaves at the same speed, and location of peak overpressure is coincident with flame front.
目的研究均质土体滑坡(已知后缘裂缝位置，未知前缘剪出口位置)运动规律。
Aim To study the movement regularity of homogeneous soil landslide with known trailing edge and undetermined shear opening.
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