摘要
通过三种不同的计算方法,考虑发动机剩余推力、气动升力、阻力及俯仰力矩的作用,对飞机刹车系统正常工作和功能部分丧失时的刹车滑跑距离进行计算,为飞机构型选择提供参考。
A methodology of landing distance calculation of aircraft normal brake mode and losing part of brake capacity mode by considering the role of engine residual thrust, aerodynamic lift, drag, pitch torque will improve the accuracy of the result. Such result can be an useful reference for the aircraft architecture selection.
出处
《民用飞机设计与研究》
2012年第B11期38-42,共5页
Civil Aircraft Design & Research
关键词
刹车
刹车滑跑距离
自适应迭代算法
非因果建模
Brake
Skid Brake Distance
Self-adaptation Iteration Algorithm
Acausal Modeling
