two-dimensional wing section 二元机翼剖面
wing section lift coefficient 翼型升力系数
segmentflügel segment wing section 扇形体翼
wing center section 机翼的中段
Wing section and survival rates as second-class cabin seats 56%.
机翼段和二等舱段座位的生还率同为56%。
The wing section is connected to the fuselage with titanium fasteners.
机翼部分用钛合金螺栓与机身连在一起。
In the second design step, improvement of wing's aerodynamic characteristic is mainly depended on the weakening of shock which reduces wave drag during the wing section optimization.
在平面形状优化基础上,在机翼容积不变约束下,再采用剖面翼型优化设计,通过机翼剖面细微变化弱化较大马赫数下的激波、减小激波阻力。
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