The first input for the Half Axel is either a small, fast pull on the lower wing or a small push on the upper.
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 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).
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。
This illustrates the initial "pop" of the lower wing. the Wind dictates how hard this input is and how fast the next input occurs.
这说明了初始作用在下翼上的弹拉的效果。风力决定了动作的力度和下一个动作的时机。
The lower wing is popped to knock the kite into a Turtle(belly up, nose away), and the same line is popped again to perform the rotation .
较低一侧的放飞线被顿拉以敲击风筝进入“躺”（机腹向上，机头向外），然后同一根线被再次顿拉以执行平转。
For plate products used in lower wing applications, increased weight savings can be achieved using selective reinforcement in DADT critical areas.
这种金属板应用于低层机翼时，在DADT这种临界领域应用选择性强化理念将会实现更多的重量节省。
The input to the lower wing has been given with the right hand and notice the pilot is ready for the larger input on the upper wing with the left hand.
施加在下翼的输入动作已经由右手完成了，注意放飞者已经准备好了用左手给出施加在上翼的更大的输入动作。
Hotel amenities, including ballrooms, function rooms, spa, gym, pool, restaurants and bar, are located on the five lower levels of the wing adjacent to the tower.
酒店的设施，包括宴会厅，活动室，水疗中心，健身房，游泳池，餐厅和酒吧，位于五在机翼附近的塔较低水平。
Sea butterfly: a swimming predatory Marine sea snail. They have two wing-like outgrowths (lower right) derived from their foot, which they continually flap to swim through the water.
海蝴蝶：一只正在游动的食肉性海蜗牛。它们拥有像翅膀一样的由足进化而来的侧翼(位于右下方)，并靠拍打侧翼在水中前行。
Maximum wing loads are significantly lower than for conventional configurations, providing weight savings.
最大翼载明显低于常规配置，提供重量节省。
To increase the whole strength and stiffness of the composite wing and to lower the manufacturing cost, the main component of the wing is employed with stitched technique.
为了提高复合材料机翼的整体强度和刚度，降低制造成本，机翼的主要结构件采用缝编技术。
Through the cyclic parameter analysis and the method of fatigue life estimation, a basis for fatigue life estimation of typical lower-wing structure is established.
这一循环参数分析和疲劳寿命估算方法为典型机翼下壁板结构的疲劳寿命估算建立了基础。
Due to the lower flight height and the slower flight speed of helicopter, Compared with the fixed wing airplane, the visual system of helicopter flight simulator has the particularity in visual scene.
由于直升机飞行高度低、飞行速度较慢，直升机飞行模拟器的视景系统具有特殊性。
HDO divides the integrated optimization of composite wing structures into two sub-problems that are easy to be solved: upper level optimization and lower level optimization.
它将复合材料翼面结构综合优化设计问题分解成两个易于求解的子问题：顶层优化设计和底层优化设计。
For lower inflow dynamic pressures, the LCO of the delta wing is caused by structural geometric nonlinearity, and the numerical results correlate well with experimental data.
在小来流动压情况下，结构几何非线性引起了切尖三角翼的LCO，计算结果和试验值吻合较好。
There are totally twelve of them here. Six ones including this one serve the higher floors 11-18 while the other six at the other wing call at the lower floors 4-10.
在这里一共有十二部，其中包括此机在内的六部前往11至18字楼的较高层，而位于另外一翼的其馀六部则停较低层的4至10字楼。
Case studies included the monitoring of the central wing and outer panel jointing area, the upper and lower pivots of main landing gears.
论文以中央翼-外翼连接区域和起落架上枢轴接头等关键部位为例，说明实施监测的方法。
The upper end of the bracket body (1) is connected with a cheek side fixed wing (2), and the lower end of the bracket body (1) is connected with a mandible fixed wing (3).
支架主体（1）的上端连接有颊侧面固定翼（2），支架主体（1）的下端连接有下颌骨固定翼（3）。
The vertical force produced by the airflow past the upper and lower surfaces of the wing.
气流流过机翼上下表面所产生的垂直力。
Examine the wings, nacelles, and upper and lower nacelle strut-to-wing fairing for fuel or other fluid leaks.
检查机翼，短舱，机身到机翼的整流装置，上下短舱有无燃油或其他液体渗漏。
Moreover, for a fixed speed, the upper and lower amplitudes of the wing-store system with uncertainty are obtained and the influence of the uncertainty is cognized on the limit cycle phase pictures.
进而可以得到一定来流速度下，具有不确定机翼外挂系统幅值的上下界，以及不确定参数对极限环相图的影响。
Moreover, for a fixed speed, the upper and lower amplitudes of the wing-store system with uncertainty are obtained and the influence of the uncertainty is cognized on the limit cycle phase pictures.
进而可以得到一定来流速度下，具有不确定机翼外挂系统幅值的上下界，以及不确定参数对极限环相图的影响。
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