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翼型加厚对桨扇性能的影响研究

徐猛 李博 邱宇宸 姜东晨 许尹

机械制造与自动化2024,Vol.53Issue(4):76-81,128,7.
机械制造与自动化2024,Vol.53Issue(4):76-81,128,7.DOI:10.19344/j.cnki.issn1671-5276.2024.04.014

翼型加厚对桨扇性能的影响研究

Study on Influence of Airfoil Thickening on Propeller Performance

徐猛 1李博 1邱宇宸 1姜东晨 1许尹1

作者信息

  • 1. 南京航空航天大学 能源与动力学院,江苏 南京 210016
  • 折叠

摘要

Abstract

In order to study the influence of airfoil thickening on the performance of propeller fan,two different thickening methods were adopted to thicken the propeller fan.NUMECA software was applied to simulate the three-dimensional flow field of the rotor fan before and after thickening,and the performance changes of the rotor fan before and after thickening were compared.The results show that the performance of rotor fan,under the same flight condition,will be decreased whether by overall airfoil thickening or by only changing the maximum airfoil thickness.Compared with the overall thickening,the performance of rotor fan will be decreased more when only changing the maximum airfoil thickness.Under the condition of different angle of attack,the larger the angle of attack,the greater the performance difference of the opposite rotor fan before and after thickening.

关键词

对转桨扇/开式转子/翼型加厚/气动性能/数值模拟

Key words

counterrotating paddle fan/open rotor/airfoil thickening/pneumatic performance/numerical simulation

分类

航空航天

引用本文复制引用

徐猛,李博,邱宇宸,姜东晨,许尹..翼型加厚对桨扇性能的影响研究[J].机械制造与自动化,2024,53(4):76-81,128,7.

机械制造与自动化

OACSTPCD

1671-5276

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