论文:2023,Vol:41,Issue(1):39-46
引用本文:
赵宾宾, 黎先平, 李杰, 张恒. 前缘角冰几何参数对翼型失速特性的影响分析研究[J]. 西北工业大学学报
ZHAO Binbin, LI Xianping, LI Jie, ZHANG Heng. Influence of geometric parameters of leading edge horn-ice on stall characteristics of airfoil[J]. Journal of Northwestern Polytechnical University

前缘角冰几何参数对翼型失速特性的影响分析研究
赵宾宾1,2, 黎先平2, 李杰1, 张恒1
1. 西北工业大学 航空学院, 陕西 西安 710072;
2. 中国商飞上海飞机设计研究院, 上海 201210
摘要:
前缘角冰不规则凸起特征和几何随机性显著,分离流场特征复杂,导致翼型失速特性发生本质变化的致因机理和关键因素仍未完全明确。针对大型客机适航审定实际需求,基于典型翼型及结冰环境,构造了一族具备不同形貌特征、几何参数彼此关联的角冰冰形。结合数值模拟方法系统分析了翼型失速特性及分离流场特征对冰形高度及角度变化的参数敏感性,归纳了冰形参数改变导致失速过程分离泡发展规律发生变化的本质影响机理,为大型客机的结冰适航取证验证工作提供了更为充分的理论依据。
关键词:    前缘角冰    翼型    冰形参数    失速特性   
Influence of geometric parameters of leading edge horn-ice on stall characteristics of airfoil
ZHAO Binbin1,2, LI Xianping2, LI Jie1, ZHANG Heng1
1. School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China;
2. COMAC Shanghai Aircraft Design and Research Institute, Shanghai 201210, China
Abstract:
The irregular characteristics and geometric randomness of horn-type ice are significant while the behaviors of separation are complex. The mechanism and factor leading to the essential change of stall performance are still not clear. According to actual requirements of airworthiness certification of a large passenger aircraft, a family of horn-type ice shapes with different parameters are constructed based on typical supercritical airfoil and icing environment. By combining with wind tunnel test and numerical simulation methods, the parameter sensitivity of airfoil stall characteristics to the change of ice height and angle is systematically analyzed and the essential influence mechanism of the ice shape parameters leading to the change of separation bubble development under stall process is summarized, which provides a theoretical basis for ice airworthiness certification of large passenger aircraft.
Key words:    leading edge horn-ice    airfoil    ice shape parameters    stall performance   
收稿日期: 2022-05-19     修回日期:
DOI: 10.1051/jnwpu/20234110039
基金项目: 国家自然科学基金(11972304)与航空科学基金(2019ZA053005)资助
通讯作者: 李杰(1969-),西北工业大学教授,主要从事设计空气动力学及计算流体力学研究。e-mail:lijieruihao@nwpu.edu.cn     Email:lijieruihao@nwpu.edu.cn
作者简介: 赵宾宾(1985-),西北工业大学博士研究生,主要从事民机结冰研究。
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参考文献:
[1] CAO Y, WU Z, SU Y, et al. Aircraft flight characteristics in icing conditions[J]. Progress in Aerospace Sciences, 2015, 74:62-80
[2] LYNCH F T, KHODADOUST A. Effects of ice accretions on aircraft aerodynamics[J]. Progress in Aerospace Sciences, 2001, 37(8):669-767
[3] BRAGG M B, BROEREN A P, BLUMENTHAL L A. Iced-airfoil aerodynamics[J]. Progress in Aerospace Sciences, 2005, 41(5):323-362
[4] 周峰, 冯丽娟, 徐超军, 等. 民用飞机适航用临界冰形的确定及验证[J]. 试验流体力学, 2016, 30(2):8-13 ZHOU Feng, FENG Lijuan, XU Chaojun, et al. Determination and verification of critical ice shape for the certification of civil aircraft[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(2):8-13(in Chinese)
[5] KIM H, BRAGG M. Effects of leading-edge ice accretion geometry on airfoil performance[C]//17th Applied Aerodynamics Conference, 1999:3150
[6] BUSCH G T, BROEREN A P, BRAGG M B. Aerodynamic simulation of a horn-ice accretion on a subscale model[J]. Journal of Aircraft, 2008, 45(2):604-613
[7] MANSHADI M D, ESFEH M K. Experimental investigation of flowfield over an iced aerofoil[J]. The Aeronautical Journal, 2016, 120(1227):735-756
[8] RAJ L P, YEE K, MYONG R S. Sensitivity of ice accretion and aerodynamic performance degradation to critical physical and modeling parameters affecting airfoil icing[J]. Aerospace Science and Technology, 2020, 98:105659
[9] 袁坤刚, 曹义华. 积冰几何特性对翼型性能影响的神经网络预测[J]. 北京航空航天大学学报, 2008(8):900-903 YUAN Kungang, CAO Yihua. Effect of ice geometry to airfoil performance using neural networks prediction[J]. Journals of Beijing University of Aerodynamics and Astronautics, 2008(8):900-903 (in Chinese)
[10] CAO Y, YUAN K, LI G. Effects of ice geometry on airfoil performance using neural networks prediction[J]. Aircraft Engineering and Aerospace Technology, 2011, 83(5):266-274
[11] 周莉, 徐浩军, 杨哲, 等. 冰脊对翼型气动特性影响的数值模拟研究[J]. 飞行力学, 2012, 30(6):489-493 ZHOU Li, XU Haojun, YANG Zhe, et al. Numerical simulation ofridgeice shapes on airfoil aerodynamics[J]. Flight Dynamics, 2012, 30(6):489-493 (in Chinese)
[12] 黄冉冉, 李栋, 刘藤, 等. 冰形表面粗糙度对翼型的失速特性影响分析[J]. 空气动力学学报, 2021, 39(1):59-65 HUANG Ranran, LI Dong, LIU Teng, et al. The effect of ice accretion roughness on airfoil stall aerodynamics[J]. Acta Aerodynamica Sinica, 2021, 39(1):59-65 (in Chinese)
[13] 郑诚毅, 东乔天, 赵宾宾, 等. 不同攻角和翼型的简化角冰特征参数的气动数值模拟[J]. 同济大学学报, 2021, 49(10):1443-1450 ZHENG Chengyi, DONG Qiaotian, ZHAO Binbin, et al. Aerodynamic numerical simulation of characteristic parameters of simplified horn ice at different angles of attack and airfoils[J]. Journal of Tongji University, 2021, 49(10):1443-1450 (in Chinese)
[14] MARONGIU C, VITAGLIANO P L, ZANAZZI G, et al. Aerodynamic analysis of an iced airfoil at medium/high Reynolds number[J]. AIAA Journal, 2008, 46(10):2469-2478
[15] STEBBINS S J, LOTH E, BROEREN A P, et al. Review of computational methods for aerodynamic analysis of iced lifting surfaces[J]. Progress in Aerospace Sciences, 2019, 111:100583
[16] POURYOUSSEFI S G, MIRZAEI M, NAZEMI M M, et al. Experimental study of ice accretion effects on aerodynamic performance of an NACA 23012 airfoil[J]. Chinese Journal of Aeronautics, 2016, 29(3):585-595
[17] LEE S, BRAGG M B. Investigation of factors affecting iced-airfoil aerodynamics[J]. Journal of Aircraft, 2003, 40(3):499-508
[18] BRAGG M B, KHODADOUST A, SPRING S A. Measurements in a leading-edge separation bubble due to a simulated airfoil ice accretion[J]. AIAA Journal, 1992, 30(6):1462-1467
[19] MIRZAEI M, ARDEKANI M A, DOOSTTALAB M. Numerical and experimental study of flow field characteristics of an iced airfoil[J]. Aerospace Science and Technology, 2009, 13(6):267-276