And this ensures that the blending surface between wing and fuselage and the long fringesurface are G-1 connected.
通过使中间辅助过渡面的边界切矢与弹身的纵向切矢一致，来保证长边条面与翼身融合面间的G-1连续性。
2
Then the forward 3-sided surface is generated based on energy minimization and is G-1 continuous contact with the missile's body and the long fringesurface.
最后利用基于物理的能量曲面造型方法构造与弹身和长边条面G-1连续的头锥过渡面。
3
The invention discloses a method for analyzing digital interference fringe and a device for detecting optical component surface shape.