Numerical study on water film flow and sheddingin ice accretion of rotating spinner
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摘要: 为了更准确地模拟旋转整流罩积冰过程,在现有三维积冰与冰层表面薄水膜流动耦合模型基础上,基于功平衡分析的方法引入了旋转部件表面水膜脱离模型,并发展了相应的计算方法,给出了水膜脱离的判定依据:当气流曳力做的功和由于离心力使水膜增加的潜能之和大于黏附功时整流罩表面的水膜会发生脱离。对旋转整流罩积冰进行数值模拟,计算结果与实验结果吻合得较好,验证了该模型的合理性和计算方法的可行性。之后分析了转速和来流速度对整流罩表面水膜脱离和积冰的影响,结果表明:转速和来流速度越大,水膜发生脱离的比例越大。在研究范围内,转速为3000r/min和6000r/min时,因水膜脱离导致积冰总量分别减少13.4%和15.8%;来流速度为40、50m/s和60m/s时,因水膜脱离导致积冰总量分别减少为12.2%、13.4%、14.2%。Abstract: In order to simulate ice accretion accurately, a water film shedding model on rotating surface was introduced with the method of work balance analysis based on the current three-dimensional coupled model of ice accretion and thin water film on ice surface. A computational methodology and a criteria of water film shedding were then presented. Water film shedding occurred when the work done by air drag force plus potential energy caused by centrifugal force was greater than adhesive work. When the method to numerical simulation of rotating spinner, the simulation results agreed well with experimental results, indicating the current model was reasonable and computational method was feasible. The effect of rotating speed and air speed on water film shedding and ice shape was also simulated. The results show that the proportion of water film shedding increased with larger rotating speed and air speed. The ice mass decreased 13.4% and 15.8% respectively due to water film shedding, when rotating speed was 3000r/min and 6000r/min.The ice mass decreased 12.2%, 13.4% and 14.2% respectively due to water film shedding, when air speed was 40m/s, 50m/s and 60m/s.
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Key words:
- rotating spinner /
- water film flow /
- water film shedding /
- centrifugal force /
- air drag force /
- ice accretion
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[1] CHAPUT M.Use of water vapor for engine deicing applications[R].Seville,Spain:2007 SAE Aircraft & Engine Icing Conference and Exhibition,2007. [2] GRAVERSEN P.Grand based measuring and warning of weather conditions in which engine icing may occur[R].Seville,Spain:2007 SAE Aircraft & Engine Icing Conference and Exhibition,2007. [3] SHAW R J,PAUL R G.The UH-1H helicopter icing flight test program:anoverview[R].AIAA-85-0338,1985. [4] BRITTON R K.A review of icing accretion data from a model rotor icing test and comparison with theory[R].AIAA-91-0661,1991. [5] BARUZZI G,TRAN P,HABASHI W G,et al.Actuator disk implementation in FENSAP-ICE,a 3-D Navier-Stokes in-flight icing simulation system progress[R].AIAA-2003-619,2003. [6] BELZ R A,BRASIER C W,MURPHY P J,et al.A turbine engine inlet viewing system[R].AIAA-86-1647,1986. [7] MCVEY O,PULLEN R.Inclement weather &aircraft engine icing[R].Seville,Spain:SAE Aircraft & Engine Icing Conference and Exhibition,2007. [8] LI Linkai,HU Hui.An experimental study of dynamics ice accretion process on aero-engine spinners[R].AIAA-2017-0551,2017. [9] 赵秋月.航空发动机进口支板及整流罩水滴撞击特性的计算分析[D].上海:上海交通大学,2011.ZHAO Qiuyue.Computational analysis of water droplet impingerment property for the inlet struct and the cone[D].Shanghai:Shanghai Jiao Tong University,2011.(in Chinese) [10] 胡娅萍.航空发动机进口部件积冰的数值模拟研究[D].南京:南京航空航天大学,2008.HU Yaping.Numerical simulation ofice accretion on aero-engine entry components[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2011.(in Chinese) [11] 王健.旋转整流罩积冰模拟实验与冰脱落轨迹数值计算研究[D].南京:南京航空航天大学,2013.WANG Jian.Experimental study of ice accretion on rotating spinner and numerical simulation of shed ices trajectory[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2013.(in Chinese) [12] 王健,胡娅萍,吉洪湖,等.旋转整流罩积冰生长与脱落过程的实验[J].航空动力学报,2014,29(6):1352-1357.WANG Jian,HU Yaping,JI Honghu,et al.Experimental of ice accretion and shedding on rotating spinner[J].Journal of Aerospace Power,2014,29(6):1352-1357.(in Chinese) [13] 胡娅萍,吉洪湖,王健,等.锥角对旋转整流罩积冰影响的模拟实验[J].航空动力学报,2014,29(3):495-503.HU Yaping,JI Honghu,WANG Jian,et al.Experiment on effect of cone angle on ice accretion of rotating spinner[J].Journal of Aerospace Power,2014,29(3):495-503.(in Chinese) [14] CHEN Ningli,JI Honghu,HU Yaping,et al.Experimental study of icing accretion on a rotating conical spinner[J].Heat and Mass Transfer,2015,51(12):1717-1729. [15] DONG W,ZHU J J,ZHENG M,et al.Numerical study of ice accretion on rotating aero-engine cone[R].Stockholm:29th Congress of the International Council of the Aeronautical Sciences,2014. [16] MU Zuodong,SHEN Xiaobin,LIN Guiping,et al.Numerical simulation for ice accretion on rotating cowling considering water film shedding[R].AIAA-2016-2187,2016. [17] ZHANG Lifen,ZHANG Meihua,ZHANG Xiaoxue,et al.Model of ice accretion on rotating cone in aero-engine[R].AIAA-2016-5059,2016. [18] 李静.发动机进口静止/旋转部件结冰及结冰实验的相似性研究[D].西安:西北工业大学,2015.LI Jing.Numerical simulation of ice accretion and study for icing scaling law on aero-engine entry components[D].Xian:Northwestern Polytechnical University,2015.(in Chinese) [19] CHEN Xi,ZHAO Qijun.Numerical simulation for ice accretion on rotors using new three-dimensional icing model[J].Journal of Aircraft,2017,54(4):1428-1442. [20] 曹广州.迎风表面三维积冰的数学模型与计算方法研究[D].南京:南京航空航天学,2011.CAO Guangzhou.Investigation of mathematic model and calulational methodology for 3D ice accretion on the up-wind surfaces[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2011.(in Chinese) [21] 陈宁立.旋转部件表面薄水膜流动与积冰的模拟方法研究[D].南京:南京航空航天大学,2018.CHEN Ningli.Research on the prediction of movement and solidification of thin water film on a rotating surface and its features[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2018.(in Chinese) [22] MIRABEDINI S M,RAHIMI H,HAMEDIFAR S,et al.Microwave irradiation of polypropylene surface:astudy on wettability and adhesion[J].International Journal of Adhesion and Adhesives,2004,24(2):163-170. [23] MURPHY A D.Computational fluid dynamics:theory,analysis,applications[M].New York:Nova Science Publishers,2011. [24] 胡坤,李振北.ANSYS ICEM CFD工程实例详解[M].北京:人民邮电出版社,2014:210-215.
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