飞机最大瞬时盘旋角速度试飞技术  

Flight Test Technology for Maximum Instantaneous Rotation Angular Velocity of Aircraft

作　　者：张奇 Zhang Qi(Aircraft Flight Test Technology Institute,CFTE,Xi'an,China)

机构地区：[1]中国飞行试验研究院飞机所,陕西西安

出　　处：《科学技术创新》2024年第8期204-207,共4页Scientific and Technological Innovation

摘　　要：最大瞬时盘旋角速度是衡量战斗机空战优势的一项重要考核指标,反映了在近距空战中驾驶员获得首次指向目标的能力。文章针对飞机最大瞬时盘旋角速度试飞技术,详细分析了国军标要求、基础理论,明确了飞机最大瞬时盘旋角速度试飞方法及试飞风险等内容,能够为飞机最大瞬时盘旋角速度试飞提供技术支持。The maximum instantaneous hovering angular velocity is an important assessment indicator for measuring the superiority of fighter jets in air combat,reflecting the pilot's ability to first point at the target in close range air combat.The article provides a detailed analysis of the requirements and basic theories of the National Military Standard for the flight test technology of the maximum instantaneous turning angular velocity of aircraft.It clarifies the flight test method and risk of the maximum instantaneous turning angular velocity of aircraft,which can provide technical support for the flight test of the maximum instantaneous turning angular velocity of aircraft.

关 键 词：盘旋 空战优势 试飞技术 风险 

分 类 号：V217.3[航空宇航科学与技术—航空宇航推进理论与工程]