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。
But the newer tower section, with its 200 rooms, was ready, as were sections of the old wing, which holds the hotel's five restaurants and its upscale shops.
酒店有200个房间的新楼已经恢复营业，老楼部分的五个餐厅以及高档商场也开业了。
A section of (wing trailing-edge) flap detached during flight probably due to material fatigue.
一段襟翼在飞行中掉落可能因材料疲乏。
Its advantage is that the relative coordinate value may be Siven conveniently for the arbitrary oblique section of wing surface.
本方法的优点是，可以方便地给出翼面类任意斜截面外形的相对坐标值。
Under unfavourable work conditions a dangerous section forms on the inner wing of the joint between sprag and grip, where the stresses are concentrated.
木材抓具的抓爪，在不利工况下的危险截面是位于撑杆与抓爪联结爪耳处的内缘，该处所受应力最大。
Pressure and velocity fields of spatial cross section on an aircraft model with strake wing and double vertical tails were measured using a seven hole probe.
采用七孔探针对一种边条翼双垂尾布局的飞机模型进行了空间压力场和速度场的测量。
The middle cerebral artery was divided into three section, the middle section was relatively longer with less branches, the surface was covered sphenoid bone greater wing.
大鼠的大脑中动脉可分三段，中段较长，分支较少，表面为蝶骨大翼覆盖。
Cracks occurred in the main weld joining the web and upper wing panel of an overhead crane girder of I-section, some of which have expanded to the structure material and even led to girder fracture.
桥式起重机采用工字形截面作为主梁，使用多年后该结构形式的主梁上翼缘板和腹板连接的主焊缝及母材多处产生裂纹，甚至发生主梁断裂事故。
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).
标准大修实施手册(SOPM) 20-10-01的内容通常在每个CMM的相关章节中的大翼部件(襟翼滑轨和襟翼滑架)的翻修部分都有具体的描述。
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).
标准大修实施手册(SOPM) 20-10-01的内容通常在每个CMM的相关章节中的大翼部件(襟翼滑轨和襟翼滑架)的翻修部分都有具体的描述。
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