修正的动力盘模型与三维模拟螺旋桨滑流比较

段中喆; 刘沛清; 屈秋林; 刘振臣

修正的动力盘模型与三维模拟螺旋桨滑流比较

北京航空航天大学航空科学与工程学院, 北京 100191

基金项目: 航空科学基金资助项目(20102351023)

详细信息

中图分类号: V224⁺.5
计量
- 文章访问数: 1917
- HTML全文浏览量: 137
- PDF下载量: 817
- 被引次数: 0
出版历程
- 收稿日期: 2012-05-22
- 修回日期: 2012-11-26
- 网络出版日期: 2013-05-31

Slipstream characters comparison of improved actuator disk model and 3D propeller numerical simulation

School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 比较用于研究螺旋桨滑流对机翼影响的4种数值模拟方法,即未进行修正的动力盘数值模拟、修正的片条理论应用于动力盘模型的数值模拟、有旋转的修正的片条理论应用于动力盘模型的数值模拟及定常三维实体螺旋桨数值模拟求解RANS(Reynolds Averaged Navier-Stokes)方程.以某半径为1.008 m三叶螺旋桨在转速为2 575 r/min,飞行速度为 66.889 m/s 工况下螺旋桨后的轴向和环向诱导系数作为评估依据进行比较,结果表明:修正的动力盘模型和三维实体模型数值模拟能预测螺旋滑流区内的流动情况,而三维实体模型能更多地反映流动细节,但是会增加计算成本,表明动力盘模型可以替代三维实体螺旋桨进行数值模拟.
- 动力盘模型 /
- 片条理论 /
- 数值模拟 /
- 滑流
Abstract: Four different propeller simulation models were compared to study the influence of propeller slipstream by solving Reynolds averaged Navier-Stokes(RANS) equations, including two prediction methods of the standard strip theory with and without rotate velocity correction applied in the actuator disk models and the uncorrected actuator disk model and 3D propeller model on a certain condition (at free stream velocity 66.889 m/s, with propeller rotation of 2 575 r/min and propeller radius 1.008 m). Results of axial and tangential velocity distribution behind the propeller show that propeller slipstream area could be predicted by the actuator disk model and the 3D propeller model when more flow details are reflected by the 3D model with more calculation cost. It all proved that the numerical simulation of 3D propeller could be replaced by the actuator disk model.
- actuator disk model /
- standard strip theory /
- numerical simulation /
- slipstream

HTML全文

参考文献(14)

[1]	Delano J B,Crigler J L.Compressibie-flow solutions for the actuator disk[R].NACA RM L53A07,1953
[2]	Malard L,Bousquet J M,Atinault O,et al.High speed testing and CFD investigations for the new generation military transport aircraft development[R].AIAA 2005-4744,2005
[3]	Veldhuis L L M,Rentema D W E.Quantitative wake surveys behind a tractor propeller-wing configuration[R].AIAA 95-3908,1995
[4]	Roosenboomet E W M.Advanced experimental and numerical validation and analysis of propeller slipstream flows[J].Journal of Aircraft,2010,47(1):284-291
[5]	Ralston J,Hultberg R.Full-envelope aerodynamics modeling of a general aviation aircraft with propeller slipstream effects[R].AIAA 2010-7922,2010
[6]	Westmoreland W S,Trameland R W,Barber J.Modeling propeller flow-fields using CFD[R].AIAA 2008-402,2008
[7]	Strawn R C.Computational modeling of hovering rotors and wakes[R].AIAA-2000-0110,2000
[8]	Wang D,Lindblad I.Characters of propeller models in Euler equations[R].AIAA 97-0402,1997
[9]	Veldhuis L L M,luuresma G W.Comparison of an actuator disk and a blade modeling approach in Navier-Stokes calculations on the SR-3 profan[R].AIAA 2000-4528,2000
[10]	Stuermer A W.Unsteady CFD simulations of propeller installation effects[R].AIAA 2006-4969,2006
[11]	Daisuke Kubo,Koji Muraoka,Noriaki Okada.High angle of attack flight of a wing in propeller slipstream mini unmanned aircraft[R].AIAA 2010-3467,2010
[12]	刘沛清.空气螺旋桨理论及其应用[M].北京:北京航空航天大学出版社,2006 Liu Peiqing,Theory and application of air propellers[M].Beijing:Beihang University Press,2006(in Chinese)
[13]	段中喆,刘沛清.某型螺旋桨滑流对机翼气动性能影响的数值研究[J].应用基础与工程科学学报,2012,20(增刊):215-225 Duan Zhongzhe,Liu Peiqing.Numerical researches on the aerodynamic characteristics of a wing influenced by the slipstream of propellers[J].Journal of Basic Science and Engineering,2012,20(Supplement):215-225(in Chinese)
[14]	段中喆,刘沛清,屈秋林.某轻载螺旋桨滑流区三维流场特性数值研究[J].控制工程,2012,19(5):836-840 Duan Zhongzhe,Liu Peiqing,Qu Qiulin.Numerical research on 3-D flow field characteristics within the slipstream of low loaded propeller[J].Control Engineering of China,2012,19(5): 836-840(in Chinese)