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滑动蒙皮变后掠无人机非定常气动特性研究

陈钱 白鹏 陈农 李锋

空气动力学学报2011,Vol.29Issue(5):645-650,6.
空气动力学学报2011,Vol.29Issue(5):645-650,6.

滑动蒙皮变后掠无人机非定常气动特性研究

Investigation on the unsteady aerodynamic characteristics of sliding-skin variable-sweep morphing unmanned aerial vehicle

陈钱 1白鹏 1陈农 1李锋1

作者信息

  • 1. 中国航天空气动力技术研究院,北京100074
  • 折叠

摘要

Abstract

In order to explore the unsteady aerodynamic characteristics and its mechanism of aircraft during shape morphing, wind tunnel experiments of a sliding-skin variable-sweep morphing unmanned aerial vehicle (UAV) were conducted, and unsteady aerodynamic characteristics were studied. The results demonstrate that; the unsteady aerodynamic characteristics curves of the UAV during shape morphing generate hysteresis loops around corresponding quasi-steady curves; the faster the UAV morphs, the greater the hysteresis effect is; when the UAV varies sweep with a speed of 7.5°/s, the value of the unsteady aerodynamic characteristics will deviate corresponding quasi-steady value by exceeding 5% ; the main reasons of the formation of the above unsteady aerodynamic characteristics may be flow-field structure hysteresis and wing additional-velocity.

关键词

变形飞机/非定常气动特性/流场结构迟滞/机翼附加速度/风洞实验/变后掠/滑动蒙皮

Key words

morphing aircraft/unsteady aerodynamic characteristics/flow field structure hysteresis/wing additional- velocity/wind tunnel experiment/variable sweep/sliding skin

分类

航空航天

引用本文复制引用

陈钱,白鹏,陈农,李锋..滑动蒙皮变后掠无人机非定常气动特性研究[J].空气动力学学报,2011,29(5):645-650,6.

基金项目

国家自然科学基金重点项目(90816026) (90816026)

空气动力学学报

OA北大核心CSCDCSTPCD

0258-1825

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