空气动力学学报2017，Vol.35Issue(1)：13-19,26,8.DOI:10.7638/kqdlxxb-2015.0013
制空型无人机的关键技术、气动布局及特性
Key technique and aerodynamic configuration characteristic of UCAV with command of the air
车竞 1何开锋 1钱炜祺1
作者信息
- 1. 中国空气动力研究与发展中心 计算空气动力研究所,四川 绵阳 621000
- 折叠
摘要
Abstract
UCAV with command of the air (UCAV-CA)is considered to be an important development branch for fighter planes or UCAVs in the future.This paper analyses the technical characteristic of UCAV-CA,and points out its two development routes,one is fighter plane unmanned and the other flying wing UCAV updating.And then,the technical and tactical demands and key techniques of UCAV-CA are studied.Furthermore,two important aerodynamic configurations including flat blend wing body with middle/small aspect ratio and flying wing body with middle/big aspect ratio are concluded,and one possible aerodynamic configuration which has (duck style)flying wing body with middle/small aspect ratio is present.Finally,the design demand to UCAV-CA of aerodynamic configuration is summarized,which is expected to bring some suggestions for designers.关键词
制空型无人机/无人战斗机/气动布局/飞翼布局/扁平融合体布局Key words
UCAV-CA/UCAV/aerodynamic configuration/flying wing configuration/flat blend wing body分类
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车竞,何开锋,钱炜祺..制空型无人机的关键技术、气动布局及特性[J].空气动力学学报,2017,35(1):13-19,26,8.
