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- full distance flight test 全程飞行试验
- Nobody thought he'd last 15 rounds, but he went the full distance. 没有人认为他会坚持15个回合，然而他终於打满了全局。
- Nobody thought he'd last 15 rounds,but he went the full distance. 个回合，然而他终于打满了全局。
- During the processing of developing antiaircraft missile armament system, miss distance is one important parameter in analying flight test data. 摘要脱靶量是防空导弹武器系统研制过程中进行飞行试验数据分析的一个重要参数。
- Participate in the flight test procedures improvement. 参与试飞程序的完善。
- Nobody thought he would last 15 rounds but he went the full distance. 谁都以为他坚持不到15个回合，可他却打完了全场。
- Long distance flight uses more fuel than car and brings pollution to the environment. 翻译：长距离的飞行耗费的能源比汽车多并带来对环境的污染。
- 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。
- Operating Instructions: Use the left mouse button click on jumping, 2 hits can be a short distance flight and landed automatically make stampede movements. 操作指南:使用鼠标左键点击跳跃,2次点击可进行短距离飞行,降落时自动做出踩踏的动作。
- 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。
- 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。
- 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。
