双孔射流对圆柱表面水滴撞击特性影响的数值分析

李峰梅; 柯鹏

doi:10.7638/kqdlxxb-2018.0022

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双孔射流对圆柱表面水滴撞击特性影响的数值分析

研究论文 | 更新时间：2026-05-28

- 双孔射流对圆柱表面水滴撞击特性影响的数值分析
- Numerical investigation on the influence of air jet on droplets impact on 3D holed cylinder
- 空气动力学学报 2019年37卷第6期页码：990-997
- 作者机构：
  
  1. 北京航空航天大学交通科学与工程学院,北京,100191
  2. 飞机/发动机综合系统安全北京市重点实验室,北京,100191
- 作者简介：
  
  李峰梅(1991-), 女, 河南洛阳人, 硕士研究生, 研究方向:发动机防冰.E-mail:13243183520@163.com
  柯鹏(1979-), 男, 湖北孝感人, 副教授, 研究方向:飞机/发动机防除冰与适航技术.E-mail:p.ke@buaa.edu.cn
- 基金信息：
  
  国家自然科学基金（51706244）
- DOI：10.7638/kqdlxxb-2018.0022
  中图分类号： V233.94
- 纸质出版：2019
- 稿件说明：
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李峰梅, 柯鹏. 双孔射流对圆柱表面水滴撞击特性影响的数值分析[J]. 空气动力学学报, 2019, 37(6): 990-997.

LI Fengmei, KE Peng. Numerical investigation on the influence of air jet on droplets impact on 3D holed cylinder[J]. 2019, 37(6): 990-997.
李峰梅, 柯鹏. 双孔射流对圆柱表面水滴撞击特性影响的数值分析[J]. 空气动力学学报, 2019, 37(6): 990-997. DOI： 10.7638/kqdlxxb-2018.0022.

LI Fengmei, KE Peng. Numerical investigation on the influence of air jet on droplets impact on 3D holed cylinder[J]. 2019, 37(6): 990-997. DOI： 10.7638/kqdlxxb-2018.0022.

摘要

对于低导热系数复合材料制作的发动机进气部件防冰问题，冲击-热气膜复合防冰技术应用前景较好，但是射流对水滴撞击影响的还缺少研究。本文以三维开双孔圆柱为对象，采用基于欧拉-欧拉框架的三维水滴撞击数值模拟方法，分析了双孔射流对水滴撞击特性的影响。研究发现，由于开孔射流与主流之间的强耦合，射流对来流水滴存在吹袭和扩散等不同作用机制，影响规律与射流强度和物面位置密切相关。针对典型水滴直径（20 μm）和来流速度（30 m/s）的工况，取沿展向六个截面及孔间中心截面的水滴运动轨迹和涡量场进行了分析。在小吹风比（0.5和1.0）时，射流影响仅限于展向近孔截面，孔间水滴撞击系数相比于无气膜工况最大降幅为7.51%。吹风比为1.5时，射流吹袭和扩散作用更强烈，孔间水滴沿展向被吹向外侧，造成近孔截面水滴量减少而远孔截面增加，孔间截面水滴撞击系数比无气膜工况最大降幅为8.95%，水滴撞击系数由展向外侧向孔间的最大降幅约17.65%。研究初步揭示了射流气膜对圆柱表面来流水滴撞击特性的影响规律和形成原因，为后续冲击-热气膜复合防冰系统的设计提供参考。

Abstract

For the anti-icing problem of the engine air induction part with low thermal conductivity composite material

the combined heat transfer method using impingement and jet air film has promising application

while there is still a lack of systematic studies of the effects of jet air film on the water droplets impingement. The numerical simulation algorithm of three dimensional water droplet impingement based on Eulerian- Eulerian method was developed and verified by experimental data from references

where the convergence of algorithm was improved with the diffusion coefficient. The droplets impingement characteristics of the three dimensional cylinder with two parallel jet holes under three different blowing ratios (0.5

1.0

and 1.5) were then studied. It is found that

the strong coupling between the jet air film and the main stream leads to different mechanisms of blowing off and diffusion between the jet air film and water droplets

which are closely related to the jet intensity and position. For typical droplet diameters (20 μm) with certain velocity (30 m/s)

the trajectory and vorticity field of water droplets at six spanwise cross-sections and one center section cross the holes were analyzed. At small blowing ratios (0.5 and 1.0)

the jet air film effect is limited to spanwise near-hole cross-sections

and the impingement coefficient of water droplets between holes is reduced by a maximum of 7.51% compared with that without air film. When the blowing ratio is increased to 1.5

the effect of jet blowing off and diffusion is stronger

and the water droplets between holes are blown outward along the extension direction

resulting in the decrease of the water droplets in the near hole section and the increase of that in the far hole section. The water droplets impingement coefficient of the cross-section between holes is reduced by a maximum of 8.95% compared with that without air film

and the water droplets impingement coefficient is reduced by a maximum of 17.65% from extending outward to between holes. In this paper

the effects and its inner mechanisms of hot jet film on the droplet impingement characteristics were analyzed

which provides a reference for the design of the hot air film anti-icing system.

关键词

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references

LYNCH F T, KHODADOUSTB A. Effects of ice accretions on aircraft aerodynamics[J]. Progress in Aerospace Sciences, 2001, 37(8): 669-767.

CAO Y H, TAN W Y, WU Z L. Aircraft icing: An ongoing threat to aviation safety[J]. Aerospace Science and Technology, 2018, 75: 353-385.

DU Y X, LI M, GUI Y W, et al. Review of thermodynamic behavior studies in aircraft icing process[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(2): 25-36. (in Chinese)

YU J, BU X Q, LIN G P, et al. Numerical simulation of a wing hot air anti-icing system in dry air conditions[J]. Acta Aerodynamica Sinica, 2016, 34(5): 562-567. (in Chinese)

SAEED F, MORENCY F, PARASCHIVOIU I. Numerical simulation of a hot-air anti-icing system[C]//Aerospace Sciences Meeting and Exhibit, 2013.

WANG C, CHANG S, WU H. Lagrangian approach for simulating supercooled large droplets' impingement effect[J]. Journal of Aircraft, 2015, 52(2): 1-14.

SANG W M, HU S H, LU T. Numerical investigation of ice accretion effects at supercooled large droplet conditions[J]. Acta Aerodynamica Sinica, 2016, 34(5): 549-555. (in Chinese)

YANG H, KE P, YANG C. Analysis of droplet impingement characteristics of aero-engine nose cone with hot air film[C]//ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition.

SHEN X B, ZHANG Z Q, LIN G P, et al. Droplet impingement calculation on complex suface of rotating part[J]. Acta Aerodynamica Sinica, 2016, 34(6): 709-713. (in Chinese)

GUO Y X, LIU Y Z, DONG W, et al. Numerical investigation on dynamic characteristics of large droplet impacting on surface[J]. Acta Aerodynamica Sinica, 2016, 34(5): 573-580. (in Chinese)

KIM J, P GARZA DENNIS, et al. Ice accretion modeling using an eulerian approach for droplet impingement[C]//51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2013.

KIND R J, POTAPCZUK M G, FEO A, et al. Experimental and computational simulation of in-flight icing phenomena[J]. Progress in Aerospace Sciences, 1998, 34(5-6): 257-345.

IULIANO E, BRANDI V, MINGIONE G. Water impingement prediction on multi-element airfoils by means of eulerian and lagrangian approach with viscous and inviscid air flow[R]. AIAA 2006-1270, 2006.

YU C, KE P, YU G, et al. Investigation of water impingement on a multi-element high-lift airfoil by Lagrangian and Eulerian approach[J]. Propulsion and Power Research, 2015, 4(3): 161-168.

ZHAO Y, YANG X L. Impingement characteristics and anti-icing heat load calculation of certain tail plane[J]. Journal of Aerospace Power, 2012, 27(11): 2402-2407. (in Chinese)

YI X, WANG K C, GUI Y W, et al. Investigation to Scheme of 2DPIV field of view[J]. Acta Aerodynamica Sinica, 2010, 28(5): 597-601. (in Chinese)

YANG S H, LIN G P, SHEN X B. Water droplet Impingement prediction for three-dimensional complex surfaces[J]. Journal of Aerospace Power, 2010, 25(2): 290. (in Chinese).

YANG J, GUO W, LOU D C. Numerical analysis of trajectories of water droplets on the anti-icing vane of an Engine[J]. China Gas Turbine Establishment, 2011, 24(1): 19-24. (in Chinese)

SHEN X B, LIN G Y, SHENG H F, et al. Analysis on three dimensional water droplets impingement characteristics of engine inlet[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(1): 1-5. (in Chinese)

JIAN G H, JIN L, NIU S W, et al. Experimental analysis of de-icing on airfoil using heated dual synthetic jet actuators[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(3): 94-100. (in Chinese).

LI Y J, LUO Z B. An experimental investigation on the process of droplet icing frosting and defrosting decing using dual synthetic jet[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(3): 27-32. (in Chinese).

KE P, YANG H Y, WANG J K, et al. Investigation of heating characteristics of aero-engine nose cone with film-heating anti-icing system[J]. Journal of Aerospace Power, 2018, 33(3): 530-539. (in Chinese)

WANG X D, GAO F, ZHU B Y, et al. Investigation on the influence of injection angle in supersonic flow with hybrid flow control[J]. Acta Aerodynamica Sinica, 2018, 36(4): 670-676. (in Chinese).

KE P, ZHANG Y, YU G F, et al. Influence of exterior hot-film on droplet impingement characteristics over aero-engine inlet strut[J]. Journal of Aerospace Power, 2017, 32(3): 621-629. (in Chinese)

LIU H, YANG J. Effect of film gap outflow on water droplets impingement characteristics of the anti-icing vane[J]. Gas Turbine Experiment and Research. 2017, 30(2): 51-57. (in Chinese)

SLATER S A, YOUNG J B. The calculation of inertransport in dilute gas-particle flows[J]. International Journal of Multiphase Flow, 2001, 27(1): 61-87.

TONG X, LUKE E. An Eulerian simulations of icing collection efficiency using a singularity diffusion model[R]. AIAA, 2003-1073, 2003.

LIU B, KE P. Analysis of droplet impingement characteristics of three dimensional cylinder[J]. Chinese Journal of Applied Mechanics, 2016, 33(3): 389-393. (in Chinese)

WIRIGO S, SRIRAMBHATLA S. An Eulerian method to calculate the collection efficiency on two and three dimensional bodies[R]. AIAA 2003-1073, 2003.

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