机轮溅水特性及对进气道吸水的影响

doi:10.7527/S1000-6893.2017.121453

Abstract

Abstract: When an airplane passes through the water standing on runways and taxiways, the water ingestion from wheel spray is a very complex process. To analyze the characteristic of water spray and its effect on engine ingestion, two methods are proposed:analogy and numerical simulation. With the input of wheel spray typical initial parameters, the two methods are applied to analyze the water ingestion characteristics of engine inlet of domestic transport A, which could be provided as airworthiness compliance evidence. The results illustrate that the inlet would not suck spray water and demonstrate its agreement to the regulation. Numerical simulation result gives the boundary condition when the water from wheel spray is ingested by the inlet engine:side splash velocity increases to over 69 m/s, and vertical splash velocity also increases to over 40 m/s.

Key words: inlet, gas-liquid two-phase flow, wheel water spray, water ingestion, airworthiness, numerical simulation, Discrete Phase Model (DPM)

CLC Number:

V228.7⁺1

YANG Chengfeng, GUO Zhaodian, DENG Wenjian. Characteristic of airplane wheel water spray and its effect on water ingestion of engine inlet[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(2): 121453-121453.

References

[1] SÁNTA I. The effect of water ingestion on the operation of the gas turbine engine[C]//ICAS 2000 Congress.Bonn:International Council of the Aeronautical Sciences, 2000:524.1-524.9.[2] Federal Aviation Administration. Water ingestion testing for turbine powered airplanes:Advisory Circular No. 20-124[S]. Washington, D.C.:Federal Aviation Administration, 2003.[3] Federal Aviation Administration. Flight test guide for certification of transport category airplanes:Advisory Circular No. 25-7[S]. Washington, D.C.:Federal Aviation Administration, 1998.[4] 中国民航总局.中国民用航空总局关于CCAR-33-R1的修订:民航总局令第109号[S]. 北京:中国民航总局, 2002:12-16. Civil Aviation Administration of China. CCAR-33-R1 revision:Civil Aviation Administration of China order-109[S].Beijing:Civil Aviation Administration of China, 2002:12-16(in Chinese).[5] 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. QI X F, ZENG T. Water ingestion certification test method of civil aircraft power system[J]. Aeroengine, 2013, 39(3):55-58(in Chinese).[6] BRIDE M,EILLIS E. An experimental investigation of the scale relations for the impinging water spray generated by a planning surface:NACA-TN-3615[R]. Washington, D. C.:NACA, 1956.[7] BARRETT R B. Drag and spray measurements from a small pneumatic tyre travelling through a water layer[R]. London:Ministry of Aviation, 1965.[8] 王传煌, 崔健勇. 民用飞机的起落架溅水试验[J].飞行试验, 1992, 4(2):36-39. WANG C H, CUI J Y. Wheel spray and aquaplaning test of civil aircraft landing gear[J]. Flight Test, 1992, 4(2):36-39(in Chinese).[9] JUSTIN D C, MARK N S. Wheel mounted water spray deflector:US7118067B2[P]. 2006-10-10.[10] 张岳青, 徐绯, 段敏鸽, 等. 飞机轮胎溅水计算方法及翻边轮胎挡水原理分析[J]. 科学技术工程, 2014, 14(6):54-59. ZHANG Y Q, XU F, DUAN M G, et al. Method for estimating the water spray of aircraft tyre and water retaining analysis of chine tyre[J]. Science Technology and Engineering, 2014, 14(6):54-59(in Chinese).[11] BARRETT R V. Research into slush drag,wheel spray and aquaplaning at bristol university using small pneumatic tyres[D]. Bristol:University of Bristol, 1971:24-30.[12] OROURKE P J, AMSDEN A A. The TAB method for numerical calculation of spray droplet breakup:SAE Technical Paper 872089[R]. Warrendale,PA:SAE International, 1987.[13] LIU A B, MATHER D, REITZ R D. Modeling the effects of drop drag and breakup on fuel sprays:SAE Technical Paper 930072[R]. Warrendale,PA:SAE International, 1993.[14] GOODEN J H M. CR spray-Impingement drag calculation of aircraft on water-contaminated runways:NLR-TP-2001-204[R]. Amsterdam:National Aerospace Laboratory NLR, 2001.[15] DAUGHERTY R H, STUBBS S M. Measurements of flow rate and trajectory of aircraft tire-generated water spray:NASA-TP-2718[R]. Washington, D. C.:NASA, 1987.[16] Engineering Sciences Data Unit. Estimation of spray patterns generated from the sides of aircraft tyres running in water or slush:83042[S]. London:Engineering Sciences Data Unit, 1998.[17] GOODEN J H M. Engine ingestion as a result of crosswind during take-offs from water contaminated runways:NLR-TP-2013-201[R]. Amsterdam:National Aerospace Laboratory NLR, 2013.[18] ZHAO K, LIU P, QU Q, et al. Numerical simulation of aircraft tire-generated spray and engine ingestion on flooded runways[J]. Journal of Aircraft, 2017, 54(5):1840-1848.[19] QU Q, ZHANG F, LIU P, et al. Numerical simulation of water spray caused by a rolling airplane tire[J]. Journal of Aircraft, 2016, 53(1):182-188.[20] ANSYS Inc. ANSYS FLUENT 14.0 user's guide[M]. Pittsburgh, PA:ANSYS Inc., 2012.

Characteristic of airplane wheel water spray and its effect on water ingestion of engine inlet

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Chang WANG, Long HE, Dongxia XU, Min TANG, Shuai MA, Ximing WU. Flow control drag reduction of hub on coaxial rigid rotor aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529084-529084.
[2]	Changxiao ZHAO, Jun DAI, Fangzheng DONG, Daojun LI. Link safety criticality balanced scheduling for airborne time-sensitive network [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 328870-328870.
[3]	Gaojie ZHENG, Xiaoming HE, Dongpo LI, Huijun TAN, Kun WANG, Zhenlong WU, Depeng WANG. Double 90° deflection inlet/volute coupling flow characteristics of tail-powered unmanned aerial vehicle [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(4): 128782-128782.
[4]	Bing WAN, Jun CHEN, Hanchen BAI. Full flow path performance design method for wide range scramjet based on equivalent thermodynamic process [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(4): 128757-128757.
[5]	Yifan WANG, Haoying CHEN, Haibo ZHANG. Inlet/engine matching of adaptive cycle engine for cruise mission [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128637-128637.
[6]	Jiang LAI, Zhaolin FAN, Qian WANG, Siwei DONG, Fulin TONG, Xianxu YUAN. Direct numerical simulation of hypersonic cone-flare model at angle of attack [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128610-128610.
[7]	Guochi GAO, Bo ZHANG, Jingze QUAN, Chong YIN, Li DING, Yubiao JIANG. Airworthiness certification technology of normal aircraft natural icing flight test [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 128531-128531.
[8]	Kailing ZHANG, Siyi LI, Yi DUAN, Chao YAN. Uncertainty quantification of parameters in SST turbulence model for inlet simulation [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729429-729429.
[9]	Hongjian ZHANG, Yanxin ZHANG, Jianjun XIONG, Zhao ZHAO, Lin RAN, Xian YI. Numerical simulation of phased array ultrasonic beam propagation characteristics in ice layer [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729289-729289.
[10]	Wang WANG, Caiyan RAO, Cong XU, Siyi LI, Yi DUAN, Jian ZHANG. Control effect of laser energy deposition on supersonic inlet flow [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729424-729424.
[11]	Yalu FU, Xianxu YUAN, Pengxin LIU, Ming YU. Statistical properties of thermodynamic fluctuations in compressible wall⁃bounded turbulence [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(9): 127217-127217.
[12]	Yi JIN, Shu SUN, Yunjie GUO, Huijun TAN, Yue ZHANG. Dual solution internal flow phenomenon and throttling characteristics of a supersonic variable inlet [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(7): 127134-127134.
[13]	Rong HAN, Wei LIU, Xiaoliang YANG. Dynamic drag reduction mechanism of self-aligned aerodisks on hypersonic aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(4): 126633-126633.
[14]	Pinpeng ZENG, Shusheng CHEN, Jinping LI, Muliang JIA, Zhenghong GAO. Numerical simulation of heat reduction on blunt-headed bodies by combined scheme of drag reduction spike and annular jets [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(22): 128407-128407.
[15]	Fenfen XIONG, Zexian LI, Yu LIU, Tangfan XIAHOU. A review of characterization methods for parameter uncertainty in engineering design based on numerical simulation [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(22): 28611-028611.