保持住这个上翼手靠前且下翼手轻微靠后的位置。
Hold this position with your top wing hand forward and your bottom wing hand slightly back.
两个下翼各有一对西纳舰队系统的L -s9.3激光炮，可以点射或连射。
The two lower wings each hold a pair of SFS L-s9.3 laser cannons which can be fired singly or linked.
拉一点下翼或送一点上翼，紧接着果断有力地拉上翼，使风筝形成画面上这样的姿态。
A small pop to the bottom wing or a small push on the upper followed by a firm pull on the upper wing to position the kite as you see it here.
紧接着的下一个输入动作是拉刚刚的下翼（以现在的姿态看是左侧机翼）这个例子用右手。
The next input coming up is pull on what was the lower wing with the right hand( in this position it's the wing to the left).
试验证明，在纵向预应力作用下的计算截面应取道床板全部截面作为主梁下翼缘共同工作。
Tests show that the cross section of the whole deck, working jointly as the lower flange of the main girder, should be taken for the calculated section subjected to longitudinal prestressing force.
Half Axel的第一个输入动作是一个小的快速的对风筝下翼的拉也可以是一个小的快速的对风筝上翼的推。
The first input for the Half Axel is either a small, fast pull on the lower wing or a small push on the upper.
方法对87例(95只眼)翼状胬肉患者行显微镜下翼状胬肉切除并做角膜缘干细胞移植，术后随访观察12 ~24个月。
Methods 87 cases (95 eyes) pterygium were excised under microscope with corneal limbus stem cell transplantation. All cases were followed. up for 12 ~ 24 month5.
目的探讨不同交变应力作用下，大鼠翼外肌成肌细胞增殖活性的变化，为交变应力下翼外肌组织的改建提供必要的基础实验数据。
Objective To investigate the effects of time varied stress on the proliferation of myoblast in rats and provide the basic experimental data for the remodeling of tissue in functional orthopaedics.
目的探讨不同交变应力作用下，大鼠翼外肌成肌细胞增殖活性的变化，为交变应力下翼外肌组织的改建提供必要的基础实验数据。
Objective To investigate the effects of time varied stress on the shape-alteration of myoblast in rats and to provide a theoretic base to determine the mechanics of myoblast in orthodontic therapy.
本文研究了将楼板置于钢梁下翼缘的新型组合结构平面刚度，并和传统的将楼板置于钢梁上翼缘的结构形式的平面刚度和极限承载力作了比较。
This paper researches the plane stiffness of new composite structure for slab on the lower flange, which is compared with the traditional structure for the slab on the top flange.
他发现，把翼消的一根羽毛转动那么一丝丝，就可以在高速下平平稳稳地来个急转弯。
A single wingtip feather, he found, moved a fraction of an inch, gives a smooth sweeping curve at tremendous speed.
丹麦科学家正在开发一种新型的风机叶片，它模拟实现了鹰翼在强紊流风力条件下的稳定性。
Danish scientists are developing a new wind turbine blade that mimics the stability found in hawk wings during highly-turbulent wind events.
立方直升机的这种配置让他可以像直升机一样盘旋，但在向前飞行时，主旋翼的转速可以将下来，让两侧的机翼提供升力，在此情况下，两台螺旋桨推进器就能发挥大作用了。
This means it can hover like a helicopter, but when flying forwards can reduce the speed of the main rotor and let the wings provide part of the lift. Its propellers give the extra oomph.
在紧急情况下，即使16个旋翼中有4个出现问题飞机也能降落。
In an emergency, it can land even if four of its 16 rotors fail.
它使用一个安装在后面的推进式螺旋桨并有一对一上一下反向旋转的主旋翼。
The X2 uses a pusher propeller mounted at the rear and has a pair of contra-rotating main rotors, one positioned above the other.
他说，来吧，把头靠在我的翼下，你可以安心地睡去。
三套加油软管被安装在了轰炸机上，一个在机身上，两翼下分别安装的吊舱各一套。
Three refueling hoses were fitted to the bomber, one from the fuselage and one each from a pod mounted under each wing.
在远古时期，这些翼龙很可能是将它们的蛋埋在湖岸边的沙滩下，以防它们的蛋宝宝被太阳晒干。
Hamipterusmost likely buried their eggs in sand along the shore of an ancient lake to prevent them from drying out.
它是由下外侧软骨外侧脚尾侧端，软组织翼，膜性鼻中隔和鼻孔槛共同构成。
It is formed by the caudal edge of the lateral crus of the lower lateral cartilage, the soft tissue alae, the membranous septum, and the sill of the nostril.
幻影2000-5翼下只有2个大挂架，空对地武器和副油箱都只能挂这两个挂架，因此对地作战时有效载重和航程两者不可兼顾。
Since there are only two hardpoints under each wing of Mirage 2000-5 for carrying both weapon and fuel tank, you can't expect keeping long voyage while carrying more weapons.
最后进行在弯矩作用下蜂窝梁翼缘对腹板的约束作用分析。
The effect of flanges restraint on the web in castellated beams under uniform moment is analyzed.
如果你想在强热气流条件下飞行，就要搞明白自己的伞翼在不同程度塌陷状况下的不同表现。
If you want to fly strong thermic conditions, you need to learn how your wing behaves after different degrees of collapses, big and small.
在传统的固定翼飞机情况下，一旦无人机在空中发射，飞行控制权主要转移到无人机的自动驾驶仪上。
In the case of conventional fixed wing aircraft, once an UAV is launched in the sky, flight authority is mainly shifted to an autopilot onboard.
太阳翼铰链组件测试系统是专门用于太阳翼铰链组件热真空环境下各种重要力学参数的测试。
A test system used in the test of key mechanical parameters of the solar wing hinge module under thermal vacuum environment was developed.
在第一部分，通过在自由声场条件下，采用单单位胞外微电极记录方法，研究了普通伏翼蝠下丘神经元基本声反应特性。
In the first section, to study the acoustic response properties of the IC in the pipistrellus abramus, single unit extracellular recording with microelectrode was used in free field conditions.
介绍了直升机在悬停状态下，求解旋翼水滴撞击特性的数值方法。
The numerical method of determining the water droplet impingement property of rotor blade in hover was studied.
基于附着流状态下的旋翼非定常翼型气动模型，给出了计算该状态下的翼型非定常升力、阻力和俯仰力矩的数值计算方法。
A numerical method is given to calculate the unsteady lift, pitching moment and drag acting on an airfoil of rotors under attached-flow conditions in a compressible flow.
基于附着流状态下的旋翼非定常翼型气动模型，给出了计算该状态下的翼型非定常升力、阻力和俯仰力矩的数值计算方法。
A numerical method is given to calculate the unsteady lift, pitching moment and drag acting on an airfoil of rotors under attached-flow conditions in a compressible flow.
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