绕轴旋转圆柱结冰特性结冰风洞试验

doi:10.7527/S1000-6893.2016.0314

飞机结冰致灾与防护专栏

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

绕轴旋转圆柱结冰特性结冰风洞试验

李岩¹, 王绍龙¹, 易贤², 周志宏², 郭龙²

1. 东北农业大学工程学院, 哈尔滨 150030;
2. 中国空气动力研究与发展中心空气动力学国家重点试验室, 绵阳 621000

收稿日期:2016-08-23 修回日期:2016-11-30 出版日期:2017-02-15 发布日期:2016-12-13
通讯作者: 李岩,E-mail:liyanneau@163.com E-mail:liyanneau@163.com
基金资助:
国家自然科学基金（51576037，11172314）；国家“973”计划（2015CB755800）

An icing wind tunnel test on icing characteristics of cylinder rotating around a shaft

LI Yan¹, WANG Shaolong¹, YI Xian², ZHOU Zhihong², GUO Long²

1. Engineering College, Northeast Agricultural University, Harbin 150030, China;
2. State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang 621000, China

Received:2016-08-23 Revised:2016-11-30 Online:2017-02-15 Published:2016-12-13
Supported by:
National Natural Science Foundation of China (51576037, 11172314); National Basic Research Program of China (2015CB755800)

摘要/Abstract

摘要：

绕轴旋转物体结冰是一种常见的结冰现象，如风力机叶片和直升机旋翼结冰等。针对该旋转模型的结冰问题，以绕轴旋转圆柱为对象，进行了结冰风洞试验研究。试验在自行设计的利用自然低温的结冰风洞系统中完成。在对结冰风洞试验能力进行验证后，对具有不同直径、转速和结冰时间的旋转圆柱结冰进行了试验，建立了旋转圆柱的结冰分析与评价方法，分析了转速、圆柱直径、结冰时间等对圆柱结冰形状主要特征量的影响规律，包括结冰面积、无因次结冰面积、驻点厚度、无因次驻点厚度、驻点偏转角、无因次结冰上下极限等，获得了旋转圆柱的结冰特性。在此基础上，通过回归正交试验设计，构建了旋转圆柱结冰的预测模型，并进行了验证与分析。研究结果可为绕轴旋转物体结冰特性研究提供参考和借鉴。

关键词: 结冰, 旋转圆柱, 结冰风洞试验, 结冰特性, 回归分析

Abstract:

Icing on the objects rotating around a shaft is a common phenomenon, such as icing on wind turbine blade and helicopter propeller. In order to investigate the icing characteristics of the rotating model, icing wind tunnel tests are carried out on the cylinder rotating around a shaft. Tests are performed in the icing wind tunnel system with natural low temperature in cold climate. The repeatability validation test is made for the icing on rotating cylinder. Icing tests are carried out on the rotating cylinder with different rotating speed, cylinder diameter and icing time. Analysis and evaluation methods for the icing characteristics of the rotating cylinder are established. The effects of these factors on the characteristics of icing shape on rotation cylinder are explored, including icing area, dimensionless ice area, stagnation thickness, dimensionless stagnation thickness, stagnation point deflection angle, and dimensionless icing upper and lower limits. The icing characteristics of the rotating cylinder are obtained. Based on the above research, the regression equations for calculating the icing characteristics of rotating cylinder are obtained through orthogonal experimental design method, and the prediction model for the rotating cylinder is developed. Comparison and verification analysis of the test and the prediction values are carried out. The research results can provide reference for the study of icing characteristics on the object rotating around a shaft.

Key words: icing, rotating cylinder, icing wind tunnel test, icing characteristics, regression analysis

中图分类号:

V211.73

李岩, 王绍龙, 易贤, 周志宏, 郭龙. 绕轴旋转圆柱结冰特性结冰风洞试验[J]. 航空学报, 2017, 38(2): 520693-520703.

LI Yan, WANG Shaolong, YI Xian, ZHOU Zhihong, GUO Long. An icing wind tunnel test on icing characteristics of cylinder rotating around a shaft[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(2): 520693-520703.

参考文献

[1] MAKKONEN L, LAAKSO T, MARJANIEMI M, et al. Modeling and prevention of ice accretion on wind turbine on wind turbines[J]. Wind Engineering, 2001, 25(1):3-21.
[2] 徐玉貌, 吕少杰, 曹义华, 等. 旋翼桨叶结冰对直升机飞行性能的影响[J]. 航空动力学报, 2016, 31(2):399-404. XU Y M, LÜ S J, CAO Y H, et al. Effects of rotor blade icing on helicopter flight performance[J]. Journal of Aerospace Power, 2016, 31(2):399-404(in Chinese).
[3] 任鹏飞, 徐宁, 宋娟娟, 等. 结冰对风力叶片影响数值的数值研究[J]. 工程热物理学报, 2015, 36(2):313-317. REN P F, XU N, SONG J J, et al. Numerical research on impact of icing on wind turbine blades[J]. Journal of Engineering Thermophysics, 2015, 36(2):313-317(in Chinese).
[4] 严晓雪, 朱春玲, 王正之.风力机冰脱落轨迹仿真研究[J]. 计算机仿真, 2015, 32(10):123-127. YAN X X, ZHU C L,WANG Z Z. Numerical simulation of ice shedding from wind turbine[J].Computer Simulation, 2015, 32(10):123-127(in Chinese).
[5] 李国之, 曹义华. 直升机旋翼结冰后的飞行品质[J]. 南京航空航天大学学报, 2011, 43(3):381-386. LI G Z, CAO Y H. Effects of rotor icing on flying qualities of helicopter[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2011, 43(3):381-386(in Chinese).
[6] MILLER T L, KORKAN K D, SHAW R J. Analytical determination of propeller performance degradation due to ice accretion[J].Journal of Aircraft, 1987, 24(11):768-775.
[7] 陈科, 曹义华, 潘星. 改进的翼型积冰数值模拟方法[J]. 航空动力学报, 2007, 22(11):1814-1819. CHEN K, CAO Y H, PAN X. An improved numerical simulation method for airfoil ice accretion[J]. Journal of Aerospace Power, 2007, 22(11):1814-1819(in Chinese).
[8] 战培国. 国外寒冷地区风力机结冰问题研究[J]. 航空科学技术, 2016, 27(2):1-6. ZHAN P G. Review of the wind turbine icing in overseas cold regions[J]. Aeronautical Science & Technology, 2016, 27(2):1-6(in Chinese).
[9] RUFF G A, BERKOWITZ B M. Users manual for the NASA lewis ice accretion prediction code (LEWICE):NASA CR-185129[R]. Washington, D.C.:NASA, 1990.
[10] TAIKI M, MASAYA S, MAKOTO Y,et al. Numerical simulation of ice accretion phenomena on rotor blade of axial blower[J]. Journal of Thermal Science, 2012, 21(4):322-326.
[11] 易贤, 王开春, 马洪林, 等. 水平轴风力机结冰及其影响计算分析[J]. 太阳能学报, 2014, 35(6):1052-1058. YI X, WANG K C, MA H L, et al. Computation of icing and its effect of horizontal axis wind turbine[J]. Acta Energiae Solaris Sinica, 2014, 35(6):1052-1058(in Chinese).
[12] 易贤, 王开春, 马洪林, 等. 大型风力机结冰过程水滴收集率三维计算[J]. 空气动力学学报, 2013, 31(6):745-751. YI X, WANG K C, MA H L, et al. 3-D numerical simulation of droplet collection efficiency in large-scale wind turbine icing[J]. Acta Aerodynamica Sinica, 2013, 31(6):745-751(in Chinese).
[13] 李国之, 曹义华, 钟国. 旋翼结冰模型与纵列式直升机平衡特性分析[J]. 北京航空航天大学学报, 2010, 36(9):1034-1037. Li G Z, CAO Y H, ZHONG G. Rotor icing model and trim characteristics analysis for tandem helicopter[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(9):1034-1037(in Chinese).
[14] 陈希, 招启军, 赵国庆. 计入离心力影响的直升机旋翼翼型结冰数值模拟[J]. 航空动力学报, 2014, 29(9):2157-2165. CHEN X, ZHAO Q J, ZHAO G Q. Numerical simulation of ice accretion on rotor airfoil of helicopter considering effects of centrifugal force[J]. Journal of Aerospace Power, 2014, 29(9):2157-2165(in Chinese).
[15] HAN Y Q,PALACIOS J, SCHMITZ S. Scaled ice accretion experiments on a rotating wind turbine blade[J]. Journal of Wind Engineering and Industrial Aerodynamica, 2010, 109:55-67.
[16] 李岩, 王绍龙, 郑玉芳, 等. 利用自然低温的风力机结冰风洞试验系统设计[J]. 实验流体力学, 2016, 30(2):54-58, 66. LI Y, WANG S L, ZHENG Y F, et al. Design of wind tunnel experiment system for wind turbine icing by using natural low temperature[J]. Journal of Experiment in Fluid Mechanics, 2016, 30(2):54-58, 66(in Chinese).
[17] RUFF G A. Quantitative comparison of ice accretion shapes on airfoils[J]. Journal of Aircraft, 2002, 39(3):418-426.
[18] 周志宏, 易贤, 郭龙, 等. 基于云雾参数误差的结冰外形修正方法[J]. 实验流体力学, 2016, 30(3):8-13. ZHOU Z H, YI X, GUO L, et al. Ice shape correction method based on the error of cloud parameters[J]. Journal of Experiment in Fluid Mechanics, 2016, 30(3):8-13(in Chinese).
[19] BRAGG M B, GREGOREK G M. Aerodynamic characteristics of airfoils with ice accretions[C]//AIAA 20th Aerospace Sciences Meeting. Reston:AIAA, 1992.
[20] 李云雁, 胡传荣. 实验设计与数据处理[M]. 北京:化学工业出版社, 2005. LI Y Y, HU C R. Experimental design and date processing[M]. Beijing:Chemical Industry Press, 2005(in Chinese).

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

绕轴旋转圆柱结冰特性结冰风洞试验

An icing wind tunnel test on icing characteristics of cylinder rotating around a shaft

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	陈勇, 孔维梁, 刘洪. 飞机过冷大水滴结冰气象条件运行设计挑战[J]. 航空学报, 2023, 44(1): 626973-626973.
[2]	黄雄, 曲仕茹, 张恒, 陈显调. 大型客机增升构型缝翼除冰状态失速特性[J]. 航空学报, 2023, 44(1): 627077-627077.
[3]	张恒, 李杰, 赵宾宾. 结冰翼型前缘下垂变弯度容冰特性改善机制[J]. 航空学报, 2023, 44(1): 627114-627114.
[4]	束珺, 徐东光, 韩志熔, 李斯, 黄雄. 结冰风洞过冷大水滴试验中混合翼设计[J]. 航空学报, 2023, 44(1): 627182-627182.
[5]	赵宾宾, 张恒, 李杰. 翼型结冰状态复杂分离流动数值模拟综述[J]. 航空学报, 2023, 44(1): 627211-627211.
[6]	马乙楗, 柴得林, 王强, 易贤, 孔满昭. 翼面结冰过程中的冰晶运动相变与黏附特性[J]. 航空学报, 2023, 44(1): 627817-627817.
[7]	牛俊杰, 桑为民, 李栋, 郝莲, 王泽林. 一种基于水滴收集量代理模型的结冰试飞空域确定方法[J]. 航空学报, 2023, 44(1): 627697-627697.
[8]	郭琪磊, 桑为民, 牛俊杰, 袁烨. 复杂气象条件下考虑结冰风险的无人机飞行策略[J]. 航空学报, 2023, 44(1): 627518-627518.
[9]	伍强, 徐浩军, 魏扬, 裴彬彬, 薛源. 结冰条件下飞机气动/运动耦合特性[J]. 航空学报, 2022, 43(8): 125566-125566.
[10]	黄平, 卜雪琴, 刘一鸣, 林贵平, 杨坤. 混合相/冰晶条件下的结冰研究综述[J]. 航空学报, 2022, 43(5): 25178-025178.
[11]	王昭力, 曾涛, 周志宏, 陈宇. TVD格式在水滴流场数值模拟中的应用[J]. 航空学报, 2022, 43(12): 627010-627010.
[12]	李浩然, 段玉宇, 张宇飞, 陈海昕. 结冰模拟软件AERO-ICE中的关键数值方法[J]. 航空学报, 2021, 42(S1): 726371-726371.
[13]	郭向东, 柳庆林, 刘森云, 王梓旭, 李明. 结冰风洞中过冷大水滴云雾演化特性数值研究[J]. 航空学报, 2020, 41(8): 123655-123655.
[14]	梁飞, 効迎春, 鲁楠, 朱峰. 电分相电弧对全向信标电磁辐射特性的分析[J]. 航空学报, 2020, 41(8): 323705-323705.
[15]	卜雪琴, 李皓, 黄平, 林贵平. 二维机翼混合相结冰数值模拟[J]. 航空学报, 2020, 41(12): 124085-124085.