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- Flight Test Directive 飞行试验指令
- Participate in the flight test procedures improvement. 参与试飞程序的完善。
- Flight Test Direction 飞行试验指南
- Research of JL8 aircraft stall and spin flight test is described in this paper. 叙述了JL8飞机失速尾旋试飞状态、试飞方法和试飞结果。
- Any flight test and wind tunnel correlation always suffers from a great number of unknowns. 在对飞行试验与风洞试验进行比较时总有大量的未知数。
- This marks the second time the NLOS-LS CLU was used in a flight test of the PAM missile. NLOS-LS为指挥官提供即时、精确响应的火力，打击移动和静止的陆地、海上目标。
- The flight test monitor and command system is main part of flight test engineering. 试飞监控与指挥系统是飞行试验工程中的重要组成部分。
- Describe the basic progression of the first flight tests. 请描述一下首飞测试的基本过程。
- In addition, preliminary proof for the half system flight test program of SITAN algorithm was discussed. 此外还对SITAN系统半 系统试飞方案作了初步的论证工作。
- The poesend problems in evaluation antiship missile flight test are pcinted out. 指出现行反舰导弹飞行试验结果评定的命中域标准存在的问题。
- Due to the mission at the Air Force Flight Test Center, it operates a great variety of aircraft. 由于在空军班机测试中心的任务，它操作飞机的一个很棒的多样性。
- I'll book you on a direct flight to London. 我将为你预订直飞伦敦的航班。
- Another strong impression is that the airplane wants to fly a lot faster than we are allowed to fly at this point in the flight test program. 另外一个深刻印象就是这架飞机总是要比我们在当前试飞进度所允许的飞行速度飞的快一点。
- Wang, Z., Li, J., Lan, C. E. and Brandon, J. M., "Estimation of Unsteady Aerodynamic Models from Flight Test Data", AIAA Paper 2001-4017, August 2001. 飞机气动力建模讲习会,地点：中华航空公司(台北松山机场)，主办单位：国立成功大学航空太空工程系，2002年12月。
- Flight test vehicles require a certain degree of wiring and installation modification to accommodate flight test equipment. 飞行试验机需要一定程度的配线和安装改动来适应飞行测试设备。
- Weapon System Demonstration Test Directive 武器系统示范试验指示
- A kind of aircraft radome checked by this method has undergone flight tests. 该方法验证的天线罩防冰装置已经经历了飞行的考验。
- In the paper the correlations of the wind tun-nel results with flight test restults,and pilot's evaluation to the flying qualities are pre-sented. 文中还给出了风洞实验和飞行试验的相关性以及飞行员对飞行品质的评估。
- 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。
- The wind tunnel and flight test investigations show that the new conception of configuration of MAV is feasible,and compared. 在此基础上,进行了柔性-刚性混合翼微型飞行器试验原理样机的飞行试验验证。
