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Mиг-23飞机尾旋试飞体会
引用本文:徐勇凌.Mиг-23飞机尾旋试飞体会[J].飞行力学,1995(3).
作者姓名:徐勇凌
作者单位:空军试飞团
摘    要:Mиг-23飞机是一种变后掠翼战斗机,它的尾旋动态及改出尾旋的方法很复杂。根据在该机上进行的四次尾旋飞行试验,叙述其尾旋进入的方法、尾旋中的动态和改出尾旋的方法。并举出三个典型的尾旋模态实例,详细记述整个尾旋过程和进行分析,说明Mиг-23飞机尾旋动态的复杂性及其表现出的特点。最后,提出了几点在判断和改出Mиг-23飞机的尾旋时应注意的事项。

关 键 词:Mиг23飞机,失速/尾旋,动态特性,改出方法

FLIGHT EXPERIENCE ABOUT SPIN FLIGHT TEST FOR Mig-23 AIRCRAFT
Xu Yongling.FLIGHT EXPERIENCE ABOUT SPIN FLIGHT TEST FOR Mig-23 AIRCRAFT[J].Flight Dynamics,1995(3).
Authors:Xu Yongling
Institution:Flight Test Regiment of China Air Force
Abstract:Mig-23 aircraft is a kind of variable sweep wing fighter.Its spin dynamicand recovery method are extremely complex. Four times stall/spin flight test has ever beenoperated by myself in Mig-23 aircraft.This paper primarily discusses the entering methodof spin, the spin dynamic and recovery method for Mig-23 aircraft.As an example,threetypical spin modallty in which the entire spin process is detailed and analyzed are introducedborder to show the complex and characteristic of spin dynamic for Mig-23 aircraft.Finaily, some important suggestion is proposed for to judge and recover the spin of Mig-23 aircraft.
Keywords:Mig-2 3 aircraft Stall/spin Dynamic performance  Recovery method
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