英德
有道
百度
谷歌
图片
维基
百科
弹翼
missile wing
- 在该系统中给出了一种基于最小二乘原理的弹翼轮廓误差评价方法。
An profile evaluating method based on least square principle is described. - YJ-62采用常轨巡航导弹布局，弹体中部的弹翼可在发射后展开，发动机进气口位于十字尾翼的稍前方。
The YJ-62 is a conventional cruise missile design, with mid-body wings which deploy following launch. The engine inlet is mounted slightly forward of the cruciform tail fins. - 提出了预先构造中间辅助面和辅助基曲面的方法，通过辅助基曲面和弹翼面上重新参数化局部基曲面间线性组合来构造翼身融合面。
The blending surface between wing and fuselage is generated by a linear combination of a reparameterized local base surface on the wing and an auxiliary baseds.
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