摘要
针对可能引起发动机停车的风险科目试飞需要,开展了战斗机空滑迫降技术研究,提出了下滑速度、最佳空滑比、180°转弯高度损失等空滑迫降关键参数的确定方法及两种空滑迫降航线的制定方法,并通过飞行试验进行了验证。该项研究对保障试飞安全有重要意义。
According to the flight test requirements of risk subjects which may cause engine shutdown, this paper carried out the research on fighter forced landing technologies,put forward the method for determining key parameters of fighter forced landing technologies such as glide speed,optimum glide ratio, height loss in 180°turn and so on. In the end,the paper put forward two methods for setting forced landing route,which were verified by the test flight. It is of great significance to guarantee flight safety.
出处
《飞行力学》
CSCD
北大核心
2013年第6期549-552,共4页
Flight Dynamics
关键词
空滑迫降
空滑比
迫降航线
forced landing
glide ratio
forced landing route
