机场污染跑道飞机轮胎的溅水问题

doi:10.7527/S1000-6893.2014.0327

固体力学与飞行器总体设计

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

机场污染跑道飞机轮胎的溅水问题

徐绯¹, 李亚南¹, 高向阳¹, 谭泽¹, 吕军², 丁伟²

1. 西北工业大学航空学院计算力学研究所, 西安 710072;
2. 上海飞机设计研究院, 上海 201210

收稿日期:2014-04-28 修回日期:2014-11-26 出版日期:2015-04-15 发布日期:2014-12-24
通讯作者: 徐绯Tel.: 029-88493705 E-mail: xufei@nwpu.edu.cn E-mail:xufei@nwpu.edu.cn
作者简介:徐绯女, 博士, 教授, 博士生导师。主要研究方向: 计算力学、断裂冲击动力学、复合材料结构设计。Tel: 029-88493705 E-mail: xufei@nwpu.edu.cn
基金资助:
航空科学基金(2013ZD53049); 国家自然科学基金(11272266)

Water sprays produced by aircraft tyres running in contaminated runway

XU Fei¹, LI Ya'nan¹, GAO Xiangyang¹, TAN Ze¹, LYU Jun², DING Wei²

1. Computation Mechanics Research Institute, School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China;
2. Shanghai Aircraft Design and Research Institute, Shanghai 201210, China

Received:2014-04-28 Revised:2014-11-26 Online:2015-04-15 Published:2014-12-24
Supported by:
Aeronautical Science Foundation of China (2013ZD53049); National Natural Science Foundation of China (11272266)

摘要/Abstract

摘要：

飞机在有积水、融雪的跑道起降时,由轮胎滑跑所产生的溅水有可能影响飞机的滑跑性能与安全。因此,积水跑道上的滑跑溅水试验是民航飞机适航审定的一个重要科目。在有限元软件LS-DYNA中对飞机轮胎溅水进行模拟,对于水粒子的模拟采用光滑粒子流体动力学(SPH)方法。针对某一具体轮胎参数首先进行了工程估算分析,接着建立了飞机轮胎的溅水分析模型,并对模型有效性进行了验证,进而分析了多种因素对轮胎溅水形态分布的影响。通过工程估算和数值计算结果的比较,发现存在临界的飞机滑跑速度,当飞机滑跑速度处于该临界值时,侧视溅水角度达到最大值。并在数值模拟中给出了不同位置溅水量相对大小的统计方法并指出轮胎翻边对溅水有显著的影响。

关键词: 飞机轮胎, 溅水, SPH, 飞溅角度, 轮胎翻边, 滑跑速度

Abstract:

The sprays produced by aircraft tyres running in water or snowmelt may affect the running performance and the safety of flights. Therefore, test for the sprays caused by the runway water is an important subject for the flight certification of an aircraft. In this paper, the process of sprays conduction is simulated by finite element software LS-DYNA, in which the water on the runway is simulated by smoothed particle hydrodynamics (SPH) method. Based on a specific tyre, engineering method is employed to study the water spray response, then numerical analysis model is founded. Results of both methods indicate that there is a critical aircraft ground speed, below which the side-spray elevation angle increases, while above which the side-spray elevation angle decreases with the increase of aircraft ground speed. In addition, the way to calculate the amount of water in different positions is given in the numerical method, the result of which also shows that tyre chine has a significant effect on the spray response under some circumstances.

Key words: aircraft tyre, water spray, SPH, spray angle, tyre chine, aircraft ground speed

中图分类号:

V226⁺.8

徐绯, 李亚南, 高向阳, 谭泽, 吕军, 丁伟. 机场污染跑道飞机轮胎的溅水问题[J]. 航空学报, 2015, 36(4): 1177-1184.

XU Fei, LI Ya'nan, GAO Xiangyang, TAN Ze, LYU Jun, DING Wei. Water sprays produced by aircraft tyres running in contaminated runway[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(4): 1177-1184.

参考文献

[1] van Es G W H, Roelen A L C, Kruijsen E A C, et al. Safety aspects of aircraft performance on wet and contaminated runways[C]//10th Annual European Aviation Safety Seminar. Amsterdam: National Aerospace Laboratory, 1998.
[2] Dreber C R, Horne B W. Ground-run tests with a bogie landing gear in water and slush, NASA TN D-3515[R]. Washington, D. C.: NASA, 1966.
[3] Qi X F, Zeng T. Water ingestion certification test method of civil aircraft power system[J]. Aeroengine, 2013, 39(3): 55-58 (in Chinese). 戚学锋, 曾涛. 民用飞机动力装置溅水试验适航验证方法[J]. 航空发动机, 2013, 39(3): 55-58.
[4] Martin C S. Hydrodynamics of tire hydroplaning, NASA R-601[R]. Washington, D. C.: NASA, 1966.
[5] Robert H D, Sandy M S. Measurements of flow rate and trajectory of aircraft tire-generated water spray, NASA Technical Paper 2718[R]. Washington, D. C.: NASA, 1987.
[6] ESDU83042 Estimation of spray patterns generated from the sides of aircraft tyres running in water or slush[S]. London: The Royal Aeronautical Society, 1998.
[7] ESDU90035 Frictional and retarding forces on aircraft tyres Part V: estimation of fluid drag forces[S]. London: The Royal Aeronautical Society, 1992.
[8] Gooden J H M. CRspray-impingement drag calculation of aircraft on water contaminated runways[C]//The 48th CASI Annual Conference. 2001.
[9] Gooden J H M. The effect of crosswind on engine ingestion during takeoffs from water contaminated runways[C]//28th International Congress of the Aeronautical Sciences. 2012.
[10] Wu H W, Chen T F, Hu C K, et al. The hydroplaning protection of the muti-wheel aircraft[J]. Civil Aircraft Design and Research, 2011(4): 62-65 (in Chinese). 吴华伟, 陈特放, 胡春凯, 等. 多轮飞机滑水保护[J]. 民用航空设计与研究, 2011(4): 62-65.
[11] Yu Z G, Li S L, Zhu Q Y. Mechanism analysis of an aircraft tire dynamic hydroplaning[J]. Journal of Air Force Engineering University: Natural Science Edition, 2004, 5(5): 9-11 (in Chinese). 余治国, 李曙林, 朱青云. 机轮动力滑水机理分析[J]. 空军工程大学学报:自然科学版, 2004, 5(5): 9-11.
[12] Zhang Y Q, Xu F, Duan M G. Method for estimating the water spray of aircraft tyre and water retaining analysis of chine tyre[J]. Science Technology and Engineering, 2014, 14(6): 54-57 (in Chinese). 张岳青, 徐绯, 段敏鸽. 飞机轮胎溅水计算方法及翻边轮胎挡水原理分析[J]. 科学技术与工程, 2014, 14(6): 54-57.
[13] Luo W K. ARJ21—the pioneer of China's civil aircraft airworthiness forensics[J]. The Big Airplain, 2013(2): 28-35 (in Chinese). 罗文凯. ARJ21——中国民机适航取证的先行者[J]. 大飞机, 2013(2): 28-35.
[14] Zang M Y, Zhu L P, Ying Z F. Simulation analysis of hydroplaning characteristics of 3-D patterned tire[J]. Science Technology and Engineering, 2009, 9(11): 2999-3002 (in Chinese). 臧孟炎, 朱林培, 应卓凡. 3-D轮胎模型滑水仿真分析[J]. 科学技术与工程, 2009, 9(11): 2999-3002.
[15] Zhu L P. Simulation of tyre skiding based on Ls-dyna[J]. China Manufacturing Industry Informatization, 2009, 38(17): 72-75 (in Chinese). 朱林培. 基于Ls-dyna的轮胎滑水特性研究[J].中国制造业信息化, 2009, 38(17): 72-75.
[16] Oh C W, Kim T W, Jeong H Y. Hydroplaning simulation for a straight-grooved tire by using FDM, FEM and an asymptotic method[J]. Journal of Mechanical Science and Technology, 2008, 22(1): 34-40.
[17] Li L S, Xie Q L, Zheng Q P, et al. Numerical simulation of contact explosion based on Lagrange, ALE and SPH[J]. Blasting, 2011, 28(1): 18-22 (in Chinese). 李利莎, 谢清粮, 郑全平, 等. 基于Lagrange、ALE和SPH算法的接触爆炸模拟计算[J]. 爆破, 2011, 28(1): 18-22.
[18] Liu G R, Liu M B. Smoothed particle hydrodynamics—a meshfree particle method[M]. Han X, Yang G, Qiang H F, translated. Changsha: Hunan University Press, 2005: 27-29 (in Chinese). Liu G R, Liu M B. 光滑粒子流体动力学——一种无网格粒子法[M]. 韩旭, 杨刚, 强洪夫, 译. 长沙: 湖南大学出版社, 2005: 27-29.
[19] Monaghan J J. Smoothed particle hydrodynamics and its diverse applications[J]. Annual Review of Fluid Mechanics, 2012, 44: 323-346.
[20] Dalrymple R A, Rogers B D. Numerical modeling of water waves with the SPH method[J]. Coastal Engineering, 2006, 53(2-3): 141-147.

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

机场污染跑道飞机轮胎的溅水问题

Water sprays produced by aircraft tyres running in contaminated runway

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 4

编辑推荐

Metrics

本文评价

[1]	刘沛清, 葛晨晖, 屈秋林. 飞机在积水跑道起降过程的溅水雾化研究进展[J]. 航空学报, 2023, 44(21): 528911-528911.
[2]	管祥善, 徐绯, 任选其, 张显鹏. 飞机轮胎溅水鸡尾流特性数值模拟[J]. 航空学报, 2019, 40(11): 122996-122996.
[3]	杨成凤, 郭兆电, 邓文剑. 机轮溅水特性及对进气道吸水的影响[J]. 航空学报, 2018, 39(2): 121453-121453.
[4]	王猛, 张立佼, 唐恩凌. 薄壁管壳高速正撞击穿孔特性的数值研究[J]. 航空学报, 2015, 36(12): 3876-3884.