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高空菱形翼布局无人机气动特性

赵炜 黄江流 贺敏 马飞 仲康

上海航天(中英文)2024,Vol.41Issue(4):36-43,8.
上海航天(中英文)2024,Vol.41Issue(4):36-43,8.DOI:10.19328/j.cnki.2096-8655.2024.04.005

高空菱形翼布局无人机气动特性

Aerodynamic Characteristics of High-altitude Diamond Joined-wing Configuration UAVs

赵炜 1黄江流 2贺敏 1马飞 1仲康1

作者信息

  • 1. 上海机电工程研究所,上海 201109
  • 2. 上海航天动力技术研究所,上海 201109
  • 折叠

摘要

Abstract

In order to obtain the long endurance advantage of unmanned aerial vehicles(UAVs)in performing special missions such as intelligence,surveillance,and reconnaissance,the diamond joined-wing configuration UAV has received great attention.At the same time,due to the high flight altitude and low flight speed,the flow has special flow phenomena such as laminar flow-separation-transition,and the flow is complex.Its aerodynamic characteristics was studied by numerical simulation in this paper.The research shows that the diamond joined-wing configuration UAV has good aerodynamic characteristics,but there is the interference between the front and after wings.As the distance between the front and after wings approaches,the more serious the air flow through the front wing is blocked,and the more serious the air flow through the after wing is downwashed.At the same time,at high angle of attack,the flow separation of the after wing is delayed due to the downwash flow,which moves the aerodynamic focus of the whole machine backward and increases the longitudinal static stability margin.

关键词

菱形翼布局/低雷诺数/气动特性/阻滞/下洗/纵向静稳定裕度

Key words

diamond joined-wing configuration/low Reynolds number/aerodynamic characteristic/blocked/downwashed/longitudinal static stability margin

分类

信息技术与安全科学

引用本文复制引用

赵炜,黄江流,贺敏,马飞,仲康..高空菱形翼布局无人机气动特性[J].上海航天(中英文),2024,41(4):36-43,8.

上海航天(中英文)

OACSTPCD

2096-8655

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