一种给定拉力分布的螺旋桨设计方法及应用

郭佳豪; 周洲; 范中允

doi:10.13224/j.cnki.jasp.2020.06.014

一种给定拉力分布的螺旋桨设计方法及应用

doi: 10.13224/j.cnki.jasp.2020.06.014

基金项目: 装备预研项目（41411020401,41411010403）；大院大所创新计划（TC2018DYDS24）

计量
- 文章访问数: 676
- HTML浏览量: 123
- PDF量: 463
- 被引次数: 0
出版历程
- 收稿日期: 2019-11-12
- 刊出日期: 2020-06-28

A method of propeller design with given thrust distribution and it’s application

School of Aeronautics,Northwestern Polytechnical University,Xi’an 710072,China

摘要

摘要: 从螺旋桨设计出发,通过设计合适的螺旋桨,得到有利的螺旋桨滑流形式,进而改善螺旋桨/机翼构型中机翼的气动特性。通过改变螺旋桨径向拉力分布控制螺旋桨滑流,提出一种根据给定拉力分布进行螺旋桨设计的方法,并验证方法的可行性。将最小能量损失设计的螺旋桨与不同拉力分布形式设计的螺旋桨应用于多螺旋桨/机翼构型中,研究螺旋桨变化对其后机翼气动特性的影响。结果表明：通过改变螺旋桨拉力分布能够改变螺旋桨滑流,进而改变后方机翼的气动特性。拉力分布较为和缓的螺旋桨,虽其本身效率有所下降,但能够对后方机翼带来增升减阻的效果,相比于最小能量损失设计结果,升阻比可提高994%。
- 螺旋桨设计 /
- 滑流 /
- 多螺旋桨/机翼 /
- 多重参考系法 /
- 混合网格
Abstract: Starting from the propeller design, a favorable propeller slipstream form was obtained by designing a suitable propeller to improve the aerodynamic characteristics of the wing in the propeller/wing configuration. The propeller slipstream was controlled by changing the radial thrust distribution of the propeller. A method of propeller design based on the given thrust distribution was proposed and the feasibility of the method was verified. Propellers designed with minimum energy loss and different thrust distributions were applied to multi-propeller/wing configuration, so as to study the effect of the propeller on the wing. Results showed that changing the propeller force distribution can change the propeller slipstream, which in turn changed the aerodynamic characteristics of the wing. The propeller with a gentle thrust distribution can increase the lift and reduce the drag on the wing, despite of its efficiency decrease. And compared with the minimum energy loss design results, the lift-drag ratio can be increased by 994%.
- propeller design /
- slipstreams /
- multi-propeller/wing /
- ,multiple reference frame /
- hybrid grid

HTML

参考文献(28)

[1]	EHAB A E,COLIN P B.Experimental investigation of the effect of propeller slipstream on boundary layer behavior at low Reynolds number［R］.AIAA-2000-4123,2000.
[2]	李征初,王勋年,陈洪,等.螺旋桨滑流对飞机机翼流场影响试验研究［J］.流体力学实验与测量,2000,14(2):44-48. LI Zhengchu,WANG Xunnian,CHEN Hong,et al.Experimental research of influence of propeller slipstream on wing flow field［J］.Experiments and Measurements in Fluid Mechanics,2000,14(2):44-48.(in Chinese)
[3]	CATALANO F M.On the effects of an installed propeller slipstream on wing aerodynamic characteristics［J］.Acta Polytechnica,2004,44(3):8-14.
[4]	MOENS F,GARDAREIN P.Numerical simulation of the propeller/wing interactions for transport aircraft［R］.AIAA-2001-2404,2001.
[5]	左岁寒,杨永.螺旋桨滑流对带后缘襟翼机翼气动特性影响的数值分析［J］.航空计算技术,2007,37(1):54-57. ZUO Suihan,YANG Yong.Numerical simulation of propeller/high-lift system interaction［J］.Aeronautical Computing Technique,2007,37(1):54-57.(in Chinese)
[6]	李博,梁德旺,黄国平.基于等效盘模型的滑流对涡桨飞机气动性能的影响［J］.航空学报,2008,29(4):845-852. LI Bo,LIANG Dewang,HUANG Guoping.Propeller slipstream effects on aerodynamic performance of turbo-prop airplane based on equivalent actuator disk model［J］.Acta Aeronautica et Astronautica Sinica,2008,29(4):845-852.(in Chinese)
[7]	STUERMER A W.Unsteady CFD simulations of propeller installation effects［R］.AIAA 2006-4969,2006.
[8]	程晓亮,李杰.螺旋桨滑流对机翼气动特性影响的方法研究［J］.科学技术与工程,2011,11(14):3229-3235. CHENG Xiaoliang,LI Jie.Unsteady computational method for the propeller/wing interaction［J］.Science Technology and Engineering,2011,11(14):3229-3235.(in Chinese)
[9]	夏贞锋,杨永.螺旋桨滑流与机翼气动干扰的非定常数值模拟［J］.航空学报,2012,32(1):76-79. XIA Zhenfeng,YANG Yong.Unsteady numerical simulation of interaction effects of propeller and wing［J］.Acta Aeronautica et Astronautica Sinica,2012,32(1):76-79.(in Chinese)
[10]	王红波,祝小平,周洲,等.太阳能无人机螺旋桨滑流气动特性分析［J］.西北工业大学学报,2015,33(6):910-920. WANG Hongbo,ZHU Xiaoping,ZHOU Zhou,et al.Aerodynamic investigation on propeller slipstream flows for solar powered airplanes［J］.Journal of Northwestern Polytechnical University,2015,33(6):910-920.(in Chinese)
[11]	王科雷,祝小平,周洲,等.低雷诺数分布式螺旋桨滑流气动影响［J］.航空学报,2016,37(9):2669-2678. WANG Kelei,ZHU Xiaoping,ZHOU Zhou,et al.Distributed electric propulsion slipstream aerodynamic effects at low Reynolds number［J］.Acta Aeronautica et Astronautica Sinica,2016,37(9):2669-2678.(in Chinese)
[12]	ZORI L A J,RAJAGOPALAN R G.Navier-stokes calculations of rotor-airframe interaction in forward flight［J］.Journal of the American Helicopter Society,1995,40(2):57-67.
[13]	O’BRIEN D,SMITH M.Analysis of rotor-fuselage interactions using various rotor models［R］.AIAA 2005-468,2005.
[14]	宋长虹,林永峰,陈文轩,等.基于动量源方法的涵道尾桨CFD分析［J］.直升机技术,2009(1):6-11. SONG Changhong,LIN Yongfeng,CHEN Wenxuan,et al.CFD analysis for the ducted tail rotor based on momentum source method［J］.Helicopter Technique,2009(1):6-11.(in Chinese)
[15]	MOORE M D,FREDERICKS B.Misconceptions of electric propulsion aircraft and their emergent aviation markets［R］.AIAA 2014-0535,2014.
[16]	徐家宽,白俊强,黄江涛,等.考虑螺旋桨滑流影响的机翼气动优化设计研究［J］.航空学报,2014,35(11):2910-2920. XU Jiakuan,BAI Junqiang,HUANG Jiangtao,et al.Aerodynamic optimization design of wing under the interaction of propeller slipsteam［J］.Acta Aeronautica et Astronautica Sinica,2014,35(11):2910-2920.(in Chinese)
[17]	王科雷,周洲,祝小平.耦合多螺旋桨滑流影响的低雷诺数机翼设计［J］.航空学报,2017,38(6):128013.1-128013.10. WANG Kelei,ZHOU Zhou,ZHU Xiaoping.Aerodynamic design of low-Reynolds-number wing taking into account the multiple propellers induced effects［J］.Acta Aeronautica et Astronautica Sinica,2017,38(6):120813.1-128013.10.(in Chinese)
[18]	ANGELO S D,BERARDI F,MINISCI E.Aerodynamic performances of propellers with parametric considerations on the optimal design［J］.The Aeronautical Journal,2002,106:313-320.
[19]	项松,王吉,张利国,等.一种高效率螺旋桨设计方法［J］.航空动力学报,2015,30(1):136-141. XIANG Song,WANG Ji,ZHANG Liguo,et al.A design method for high efficiency propeller［J］.Journal of Aerospace Power,2015,30(1):136-141.(in Chinese)
[20]	梁撑刚,郁新华,龚军锋.一种无人机螺旋桨的快速优化设计方法［J］.航空计算技术,2017,47(2):76-79. LIANG Chenggang,YU Xinhua,GONG Junfeng.A quick approach to optimum design of UAV propeller［J］.Aeronautical Computing Technique,2017,47(2):76-79.(in Chinese)
[21]	焦俊,宋笔锋,张玉刚,等.高空飞艇螺旋桨优化设计与气动性能车载试验［J］.航空动力学报,2017,32(1):196-202. JIAO Jun,SONG Bifeng,ZHANG Yugang,et al.Optimal design and truck-mounted testing of aerodynamic performance for the propeller of high altitude airship［J］.Journal of Aerospace Power,2017,32(1):196-202.(in Chinese)
[22]	KWON H I,YI S,CHOI S,et al.Design of efficient propellers using variable-fidelity aerodynamic analysis and multilevel optimization［J］.Journal of Propulsion and Power,2015,31(4):1057-1072.
[23]	刘芳,杜绵银,岳良明,等.高空低雷诺数高效螺旋桨设计［C］∥第3届中国航空科学技术大会论文集.北京:中国航空学会,2017:15-21.
[24]	PATTERSON M D,BORER N K,GERMAN B J.A simple method for high-lift propeller conceptual design［R］.San Diego,US:American Institute of Aeronautics and Astronautics,2016.
[25]	范中允,周洲,祝小平.一种可任意给定环量分布的螺旋桨设计方法［J］.航空动力学报,2019,32(2):434-441. FAN Zhongyun,ZHOU Zhou,ZHU Xiaoping.A design method for propeller with arbitrary circulation distribution［J］.Journal of Aerospace Power,2019,32(2):434-441.(in Chinese)
[26]	DRELA M.QPROP formulation［R］.Boston:Massachusetts Institute of Technology,2006.
[27]	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.
[28]	郭佳豪,周洲,范中允.一种耦合CFD修正的螺旋桨快速设计方法［J］.航空学报,2020,41(2):123216.1-123216.10.