航空拖靶系统大长度拖缆飞行参数计算与分析  

Calculation and Analysis on Flight Parameters of Towlinewith Large Length in Aerial Tow Target System

作　　者：李世秋[1] 安佳宁[1] 田新锋[1] 

机构地区：[1]中国人民解放军92419部队

出　　处：《航空计算技术》2014年第4期10-12,共3页Aeronautical Computing Technique

摘　　要：针对航空拖靶系统中大长度拖缆张力、下沉量等参数设计问题,给出了计算方法。结合某拖靶系统大长度拖缆的设计,对拖缆进行了多种结构组成状态下的飞行参数计算和对比分析,给出了优化后的设计结果,并应用于实际产品。经飞行验证,取得了满意的效果。Including tension and subsidence , parameters design problem of towline with large length of aerial tow target system is studied ,and the calculation method is also provided .Combined with the design of the towline with large length of a aerial tow target system ,calculation and analysis of flight parameters of this towline is completed in a variety of combinations of state .The final optimized design results are provided and applied to the actual product ,and the actual flight tests obtained satisfactory effect .

关 键 词：航空拖靶 拖缆 大长度 飞行参数 

分 类 号：O242[理学—计算数学]