The flight from Changzhou to Beijing witnesses a lowest flight load of about 27 percent.
从常州至北京的航班见证了27%的最低上座率。
This text introduces test technology solutions of Z11 flight load test of rotor system dynamic components.
本文介绍了直11型直升机旋翼系统动部件飞行载荷测量技术及方案。
Helicopter flight load test of rotor system dynamic components is the key part of flight load test of the whole aircraft, and is also the basis of helicopter life reliability calculations.
直升机旋翼系统动部件飞行载荷测量是全机飞行载荷测量的关键，也是直升机寿命可靠性工作的基础。
It is an important half hardware-in-loop simulation equipment, which is often used to simulate the aerodynamic torque load on the missile rudder or elevon actuators in the flight.
它是地面半实物仿真系统中的一种重要专用设备，用来模拟飞行器舵机在飞行过程中所承受空气动力力矩载荷。
Restarting the WebSphere Application Server servant region causes all in-flight transactions to be rolled back, resulting in extra load on the database.
重新启动WebSphereApplicationServer服务区域将导致所有正在进行的事务回滚，从而会给数据库造成额外的负载。
Through adjusting the above structure and performance parameters, rational flight parameters can be decided, which can ensure the safe helicopter mission operations of the slung-load flight.
通过对上述结构参数、性能参数的调节，可确定合理、经济的飞行参数，保证安全、高效的完成直升机机外吊挂飞行运输任务。
Therefore, correct calculation of the load on engine mount is full of great significance in aircraft design and flight safety.
因此，如何准确计算发动机固定装置的载荷，对飞机的设计乃至其飞行安全都有着重要意义。
According to flight feature and transitional thermal load value, scheme of temperature adjusting system of electronic equipment cabin was presented.
根据高空高速飞行特点及瞬态热载荷值，确定仪器设备舱调温系统方案。
To solve the problem of minimum time-to-climb, building a dynamic model of motion in the vertical direction and taking the flight mode as the linear load control.
以飞机在垂直平面的运动方程为基础，采用线性时间负荷控制的飞行模式，提出了求解飞机最短时间爬升轨迹的格点搜寻算法。
There is a larger effect of flow Angle of attack caused by high altitude wind on aerodynamic load and flight environment in rocket flighting.
高空风引起的气流攻角对火箭飞行中的气动载荷和飞行环境有较大的影响。
Airplane tail loads are difficult to determine accurately by means of model tests and theoretical analysis. In order to obtain reliable tail load data, it should be determined by flight tests.
用分析和模型试验方法难以确定可靠的尾翼载荷，所以要求通过飞行试验获取尾翼载荷数据，但因测载技术复杂，精确地测定尾翼载荷亦是困难的。
The power spectrum density (PSD) function is important in gust load flight experiment data analysis.
功率谱密度（PSD）函数在阵风载荷飞行试验数据分析中占有重要的地位。
An analysis of flight test results was conducted to explain the effects of winglets on aerodynamic load, control-stability and performances.
本文对翼尖小翼的飞行试验结果进行了分析，试图说明它对飞机的气动载荷、操稳特性及飞行性能的影响。
Persisted load flight simulator is a new simulator. In order to exactly control the motion system of the simulator, the calculation problem of pilot three-shaft acceleration load must be solved.
持续载荷飞行仿真平台是一种新型飞行模拟器，为了能够精确控制该模拟器的运动系统，需要解决飞行员的三轴加速度过载的计算问题。
When targets flight with zero load-factor, it is a changeable proportional factor guidance law.
当目标作非机动飞行时，最优制导律是变比例系数的比例制导。
Closely monitor pre-flight check and load factorfor analysis and forecast.
密切关注航前检查，运载因素，以便分析及预测。
Result show: this earth magnetic field orientation sensor can be used to detect attitude of high-load rotating flight body.
结果表明：该地磁方位传感器可应用于高过载旋转飞行体的姿态测量。
Then, a sequence of half-cycle is drawn from the matrix to construct a flight by flight random load spectrum.
然后从矩阵中抽取半循环序列，构成飞-续-飞随机谱。
In order to carry out high G-load flight training on the ground, research on new principles of G-load simulation for a novel sustained-G flight simulator (SGFS) is necessary.
为了能够在地面开展高过载的飞行员飞行训练，需要对新型持续载荷飞行模拟器(SGFS)持续性过载模拟的新原理进行研究。
Yesterday (19) first flight was carrying 121 passengers, load factor reached 95%.
昨天（19日）首航航班共载有121名旅客，客座率达到了95%。
Yesterday (19) first flight was carrying 121 passengers, load factor reached 95%.
昨天（19日）首航航班共载有121名旅客，客座率达到了95%。
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