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基于激励盘理论的螺旋桨滑流数值模拟研究
引用本文:夏贞锋,罗淞,杨永.基于激励盘理论的螺旋桨滑流数值模拟研究[J].空气动力学学报,2012(2):219-222,232.
作者姓名:夏贞锋  罗淞  杨永
作者单位:西北工业大学翼型叶栅空气动力学国防科技重点实验室
摘    要:针对螺旋桨滑流流动复杂、非定常数值模拟难度大的问题,对激励盘模型进行深入研究,提高其对滑流模拟的精度。首先根据非定常数值模拟单独螺旋桨流动结果确定激励盘载荷。分析了考虑旋向载荷分布对滑流数值模拟的重要性。采用激励盘模型得到的定常滑流速度分布与螺旋桨非定常滑流的时间平均结果非常吻合,且采用激励盘理论能够明显地缩短模拟时间,在工程应用中具有很大的优势。

关 键 词:螺旋桨  滑流  激励盘  非定常

Numerical simulations of propeller slipstream flows using actuator disk theory
XIA Zhen-feng,LUO Song,YANG Yong.Numerical simulations of propeller slipstream flows using actuator disk theory[J].Acta Aerodynamica Sinica,2012(2):219-222,232.
Authors:XIA Zhen-feng  LUO Song  YANG Yong
Institution:(National Key Laboratory of Science and Technology on Aerodynamic Design and Research, Northwestern Polytechnical University,Xi’an 710072,China)
Abstract:The flow around propeller is very complex,and the unsteady simulation method costs too much to handle it.To overcome this,actuator disk based on the load distribution of rotating blades simulated by unsteady method is presented.Analysis of the introduction of rotational velocity jump causing the swirl is conducted for the simulation of slipstream.The axial and tangential velocities in the slipstream simulated using actuator disk model agree well with the time-averaged results from unsteady simulation.Additionally,the actuator disk theory cuts down the simulation time,which is appreciated in engineering.
Keywords:propeller  slipstream  actuator disk  unsteady
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