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攻角对螺旋桨非定常特性的影响分析
引用本文:曾卓雄,张永祺,吴清.攻角对螺旋桨非定常特性的影响分析[J].上海电力学院学报,2019,35(1):16-20,42.
作者姓名:曾卓雄  张永祺  吴清
作者单位:上海电力学院能源与机械工程学院;南昌航空大学飞行器工程学院
基金项目:国家自然科学基金(51266013);航空科学基金(2013ZB56002,2013ZB56004)。
摘    要:为了分析入流速度攻角的连续变化对螺旋桨非定常特性的影响,应用滑移网格技术对螺旋桨运动进行了数值分析。结果表明:螺旋桨的时均拉力会随攻角的增大而增加;对于各单独叶片而言,向下运动时,随着攻角的增大,拉力会逐渐增加,向上运动时,拉力则会减小;在特定方位角时,随着攻角的增大,桨叶前端的轴向速度会略微增大,桨叶后端的轴向速度在小攻角时也会发生略微的变化,但在攻角较大时变化较明显;随着攻角的增大,桨叶所受到的周期性非定常载荷的波动会逐渐加剧。

关 键 词:攻角|螺旋桨|滑移网格技术|非定常数值分析
收稿时间:2018/4/13 0:00:00

Effect of Attack Angle on Propeller Unsteady Characteristics
ZENG Zhuoxiong,ZHANG Yongqi and WU Qing.Effect of Attack Angle on Propeller Unsteady Characteristics[J].Journal of Shanghai University of Electric Power,2019,35(1):16-20,42.
Authors:ZENG Zhuoxiong  ZHANG Yongqi and WU Qing
Affiliation:School of Energy and Mechanical Engineering, Shanghai University of Electric Power, Shanghai 200090, China,School of Energy and Mechanical Engineering, Shanghai University of Electric Power, Shanghai 200090, China and Aircraft Engineering College, Nanchang Hang Kong University, Nanchang 330063, China
Abstract:In order to analyze propeller unsteady characteristics induced by attack angle, sliding mesh method is utilized to simulate propeller moving. The results show that time-averaged thrust of propeller grows with the increase of attack angle. For isolated blades, when blade moves down, thrust is increased gradually with the increase of attack angle, and when blade moves up, it is reduced gradually. At a special angle, axial velocity of the front of propeller increases slightly, and axial velocity of the propeller back also increases slightly when attack angle is small, but it changes obviously when attack angle is large. The periodic unsteady load of blade is exacerbated at attack angle.
Keywords:attack angle  propeller  sliding mesh  unsteady numerical analysis
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