|Table of Contents|

Effects of momentum ratio on atomization characteristics of internal mixing gas-liquid injector(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2019年05期
Page:
66-73
Research Field:
研究与设计
Publishing date:

Info

Title:
Effects of momentum ratio on atomization characteristics of internal mixing gas-liquid injector
Author(s):
YANG Guohua12 ZHANG Botao2 ZHOU Lixin2 WANG Kai2
(1.Science Technology on Combustion, Internal Flow and Thermal-structure Laboratory,Northwestern Polytechnical University,Xi’an 710072, China; 2.Science and Technology on Liquid Rocket Engines Laboratory,Xi’an Aerospace Propulsion Institute, Xi’an 710100,
Keywords:
internal mixing gas-liquid injector atomization adaptive mesh refinement Gerris
PACS:
V430.34
DOI:
-
Abstract:
In order to research the effects of liquid-gas momentum ratio on atomization characteristics of internal mixing gas-liquid injector, the internal mixing gas liquid injector with two jet holes was numerically computed under various liquid-gas momentum ratio by the VOF method and adaptive mesh refinement algorithm based on Gerris.The results show that the characteristics of the whole spray process are captured accurately in Gerris, which consists of column distortion,bending and disintegrating into droplets.The computational results are basically in good agreement with the breakup process images in experiment.The spatial distributions of droplets were obtained and the droplets SMD of full flow field is 50~60 μm.When liquid-gas momentum ratio is small, the liquid jets of internal mixing gas liquid injector do not collide with each other, and the atomization mechanism is pneumatic atomization.With the increase of the liquid-gas momentum ratio, two liquid jets’ breakup length and penetration depth are increased, and liquid jets collide, at that time atomization mechanism is pneumatic atomization and impact atomization.

References:

[1] 杨立军, 富庆飞.液体火箭发动机推力室设计[M].北京: 北京航空航天大学出版社, 2013.
[2] 刘静, 徐旭. 高速气流中横向液体射流雾化研究进展[J].力学进展, 2009, 39(3): 273-283.
[3] 林宇震, 李林, 张弛, 等.液体射流喷入横向气流混合特性研究进展[J].航空学报, 2014, 35(1): 46-57.
[4] WU P K, KEVIN A.Breakup processes of liquid jets in subsonic crossflows:AIAA 1996-3024[R].USA:AIAA,1996.
[5] FULLER R P, WU P K, KIRKENDALL K A, et al.Effects of injection angle on atomization of liquid jets in transverse airflow[J].AIAA Journal, 2000, 38(1): 64-72.
[6] WU P K, LIN K C, JACKSON T. Effects of flow initial conditions on spray characteristics with and without crossflows[C]//44th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006.
[7] AVULAPATI M M, RAYAVARAPU V R.Experimental studies on air-assisted impinging jet atomization[J].International Journal of Multiphase Flow, 2013, 57: 88-101.
[8] XIA Y, KHEZZAR L, ALSHEHHI M, et al.Droplet size and velocity characteristics of water-air impinging jet atomizer[J].International Journal of Multiphase Flow, 2017, 94: 31-43.
[9] 李佳楠, 费俊, 周立新, 等.工质粘性对两股射流撞击雾化特性影响试验研究[J].火箭推进, 2015, 41(2): 43-49.LI J N, FEI J, ZHOU L X, et al.Experimental study of effect of working fluid viscosity on atomization characteristics of a pair of impinging jets[J].Journal of Rocket Propulsion, 2015, 41(2): 43-49.
[10] LAI W H, HUANG T H, JIANG T L, et al.Effects of fluid properties on the characteristics of impinging-jet sprays[J].Atomization and Sprays, 2005, 15(4): 457-468.
[11] 仝毅恒.横向气流中液体射流喷注特性和破碎过程研究[D].长沙: 国防科学技术大学, 2012.
[12] FARVARDIN E, DOLATABADI A.Breakup simulation of elliptical liquid jet in gaseous crossflow[C]//42nd AIAA Fluid Dynamics Conference and Exhibit.Reston, Virigina: American Institute of Aeronautics and Astronautics, 2012.
[13] PAI M, PITSCH H, DESJARDINS O.Detailed numerical simulations of primary atomization of liquid jets in crossflow[C]//47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.Reston, Virigina: American Institute of Aeronautics and Astronautics, 2009.
[14] 李佳楠, 费俊, 杨伟东, 等.直流互击式喷注单元雾化特性准直接数值模拟[J].推进技术, 2016, 37(4): 713-725.
[15] 王凯, 杨国华, 李鹏飞, 等.基于Gerris的离心式喷嘴锥形液膜破碎过程数值模拟[J].推进技术, 2018, 39(5): 1041-1050.
[16] 杨国华, 王凯, 张民庆, 等.基于树形自适应网格的旋流液膜雾化过程仿真[J].推进技术, 2018, 39(3): 556-564.
[17] 王凯,李鹏飞,杨国华,等. 相邻离心式喷嘴液膜撞击雾化过程仿真[J].推进技术,2017,38(2):408-415.
[18] 张波涛, 张友平, 张民庆.射流在不可压气流中破碎过程高精度数值仿真[J].火箭推进, 2018, 44(1): 59-66.ZHANG B T, ZHANG Y P, ZHANG M Q.High-precision numerical simulation of breakup processes of liquid jet in incompressible airflow[J].Journal of Rocket Propulsion, 2018, 44(1): 59-66.
[19] POPINET S.Gerris: a tree-based adaptive solver for the incompressible Euler equations in complex geometries[J].Journal of Computational Physics, 2003, 190(2): 572-600.

Memo

Memo:
-
Last Update: 2019-10-25