使用反推力时飞机着陆滑跑距离的换算  

Conversion Method of Landing Distance under Reverse-Thrust Conditions

作　　者：黄文静[1] 吴密翠[1] 周晓飞[1] 

机构地区：[1]中国飞行试验研究院飞机所,陕西西安710089

出　　处：《飞行力学》2003年第3期56-58,共3页Flight Dynamics

摘　　要：以装有反推力装置的某型飞机为研究对象,对其着陆滑跑距离向标准条件换算的方法进行了研究,给出了换算公式,并应用该方法将该机的实际试飞结果向标准条件进行了换算。结果表明,换算方法是正确的,该方法对其它带有反推力装置飞机的着陆滑跑距离向标准条件换算亦具有一定的参考价值。A method of converting the landing distance under reversethrust conditions into that landing distance under standard conditions is developed for aircraft equipped with a reversethrust device, and a conversion formula is derived and provided in this paper. On the basis of this, taking a certain type aircraft as an example, this method is used to convert the actual flight test results into those under standard conditions. The conversion result shows that the conversion method is correct. It can be used as a reference for converting the landing distance of aircraft with the reversethrust device into that under standard conditions.

关 键 词：反推力 飞机 着陆滑跑距离 计算 换算公式 

分 类 号：V212.131[航空宇航科学与技术—航空宇航推进理论与工程]