And this ensures that the blending surface between wing and fuselage and the long fringe surface 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
Standard Overhaul Practices Manual (SOPM) 20-10-01 generally is specified in each CMM section for the rework of wing components (e. g., flap tracks, flap carriages).