In this paper a relaxed static stability (RSS) fighter F16 is taken as an example to discuss deep stall corridor characteristics.
以放宽静稳定性（RSS）战斗机F-16为例，讨论了深失速走廊特性。 利用具有非线性气动力的简化运动方程，分析了飞机深失速特性；
This new technique allows a comfortable and controllable rapid descent without the risk of experiencing a "cravat" or "deep stall".
这项新技术在达致舒适可控地快速消高目的同时，完全避免了“夹叶插页”和“深度失速”地风险。
But cutting too deep, too fast will stall the recovery.
但如果削减赤字过激过猛则会拖累复苏的步伐。
Finally, the main factors that influence the deep - stall recovery characteristics are analyzed.
最后分析了影响深失速改出特性的主要因素。
To detect stall inception signal before the whole compressor running into deep rotating stall, a method based on averaged numerical difference is developed to detect short length scale disturbance.
为在压气机整机进入深度失速前检测到失速起始信号，提出了一种基于平均数值差分的短周期扰动检测方法。
To detect stall inception signal before the whole compressor running into deep rotating stall, a method based on averaged numerical difference is developed to detect short length scale disturbance.
为在压气机整机进入深度失速前检测到失速起始信号，提出了一种基于平均数值差分的短周期扰动检测方法。
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