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高空菱形翼布局无人机气动特性

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为了获取无人机执行情报、监视和侦察等特种任务时的长航时优势,菱形翼布局无人机受到了大家的极大关注.高空菱形翼布局无人机通过前后翼搭接,能够有效增加整机展弦比,同时由于飞行高度高,飞行速度低,流动存在层流-分离-转捩等特殊流动现象,流动具有复杂性.本文采用数值模拟方法,对菱形翼布局无人机在低雷诺数下的气动特性进行了研究.结果表明:菱形翼气动布局具有较好的气动特性,存在着前后翼相互干扰的问题.随着前后翼距离靠近,前翼受阻滞、后翼受下洗效应越严重;同时,在大迎角下,后翼受前翼下洗影响流动分离延迟,使整机气动焦点后移,纵向静稳定裕度增大.
Aerodynamic Characteristics of High-altitude Diamond Joined-wing Configuration UAVs
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.

diamond joined-wing configurationlow Reynolds numberaerodynamic characteristicblockeddownwashedlongitudinal static stability margin

赵炜、黄江流、贺敏、马飞、仲康

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上海机电工程研究所,上海 201109

上海航天动力技术研究所,上海 201109

菱形翼布局 低雷诺数 气动特性 阻滞 下洗 纵向静稳定裕度

2024

上海航天(中英文)
上海航天技术研究院

上海航天(中英文)

CSTPCD
影响因子:0.166
ISSN:2096-8655
年,卷(期):2024.41(4)