Numerical simulation of the primary breakup of fuel jet with incoming positive velocity gradient

Tao Zhang , Weimin Wang , Zhenghuan Li , Haijun Zhang , Haiqiao Wei , Rundong Li , Chang Zhai

Green Energy and Resources ›› 2024, Vol. 2 ›› Issue (3) : 100090

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Green Energy and Resources ›› 2024, Vol. 2 ›› Issue (3) : 100090 DOI: 10.1016/j.gerr.2024.100090
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Numerical simulation of the primary breakup of fuel jet with incoming positive velocity gradient

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Abstract

To study the breakup process of fuel jets in air crossflow with a positive velocity gradient, the Volume of Fluid (VOF) method and adaptive grid technology are combined to simulate the two-phase flow of gas and liquid. A comparative analysis is conducted on the breakup and corresponding flow characteristics of direct fuel jets under uniform and positive velocity gradient airflow. The simulation results demonstrate that the morphological changes of the fuel column are caused by factors such as gas-liquid shear and asymmetric airflow vortices. The fuel jet undergoes primary breakup, which mainly contains columnar and surface breakup. The columnar breakup is dominated by Rayleigh-Taylor (R-T) instability, while the surface breakup is dominated by Kelvin-Helmholtz (K-H) instability. Compared with uniform flow, the expansion angle in the positive velocity gradient incoming flow increases by an average of 9.2%, and the wavelength of the surface wave increases by an average of 34%.

Keywords

Positive velocity gradient / Crossflow / Primary breakup / Numerical simulation / Vortex

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Tao Zhang, Weimin Wang, Zhenghuan Li, Haijun Zhang, Haiqiao Wei, Rundong Li, Chang Zhai. Numerical simulation of the primary breakup of fuel jet with incoming positive velocity gradient. Green Energy and Resources, 2024, 2(3): 100090 DOI:10.1016/j.gerr.2024.100090

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CRediT authorship contribution statement

Tao Zhang: Writing - review & editing, Writing - original draft, Methodology, Investigation, Conceptualization. Weimin Wang: Writing - review & editing, Writing - original draft, Methodology, Investigation, Conceptualization. Zhenghuan Li: Writing - review & editing, Writing - original draft, Methodology, Investigation, Conceptualization. Haijun Zhang: Writing - review & editing, Writing - original draft, Methodology, Investigation, Conceptualization. Haiqiao Wei: Writing - review & editing, Writing - original draft, Methodology, Investigation, Conceptualization. Rundong Li: Writing - review & editing, Writing - original draft, Methodology, Investigation, Conceptualization. Chang Zhai: Writing - review & editing, Writing - original draft, Methodology, Investigation, Conceptualization.

Declaration of competing interest

The authors declare no competing financial interest.

Acknowledgements

This work was supported by National key research and development plan project (Grant No.2023YFC3707300), Special project of National Natural Science Foundation (Grant No. T2341001), Liaoning Revitalization Talents Program (XLYC2008013) and the fundamental research funds for the universities of Liaoning province (NO.20240163). Thanks to the help of the college and the fund, all authors were able to complete this work with high-performance computing services.

References

[1]

Anderson, T.J., Proscia, W., Cohen, J.M., 2001. Modulation of a Liquid-Fuel Jet in an Unsteady Cross-Flow. Paper Presented at the ASME Turbo Expo 2001: Power for Land, Sea and Air. https://doi.org/10.1115/2001-GT-0048.

[2]

Becker, J., Hassa, C., 2002. Breakup and atomization of a kerosene jet in crossflow at elevated pressure. Atomization Sprays 12 (1-3), 49-67. https://doi.org/10.1615/AtomizSpr.v12.i123.30.

[3]

Becker, J., Hassa, C., 2003. Liquid fuel placement and mixing of a generic aeroengine premix module at different operating conditions. J. Eng. Gas Turbines Power 125 (4), 901-908. https://doi.org/10.1115/1.1587741.

[4]

Brackbill, J.U., Kothe, D.B., Zemach, C., 1992. A continuum method for modeling surface tension. J. Comput. Phys. 100 (2), 335-354. https://doi.org/10.1016/0021-9991(92)90240-Y.

[5]

Chen, T.H., Smith, C.R., Schommer, D.G., Nejad, A.S., 1993. Multi-zone Behavior of Transverse Liquid Jet in High-Speed Flow. Paper Presented at the 31st AIAA Aerospace Sciences Meeting and Exhibit. https://doi.org/10.2514/6.1993-453.

[6]

Deng, T., Yuan, C., 2019. Liquid jet breakup in shear-laden mode air crossflow. J. Civel Aviat. Univ. China 37 (6), 18-23.

[7]

Edward, A., Kush, J., Joseph, A., Schetz, 1973. Liquid jet injection into a supersonic flow. AIAA J. 11 (9), 1223-1224. https://doi.org/10.2514/3.50567.

[8]

Elshamy, O., Tambe, S., Cai, J., Jeng, S.M., 2006. Structure of liquid jets in subsonic crossflow at elevated ambient pressures. Paper Presented at the. 44th AIAA Aerospace Sciences Meeting and Exhibit. https://doi.org/10.2514/6.2006-1224.

[9]

Elshamy, O., Tambe, S., Cai, J., Jeng, S.M., 2007. Excited Liquid Jets in Subsonic Crossflow. Paper Presented at the 45th AIAA Aerospace Sciences Meeting and Exhibit. https://doi.org/10.2514/6.2007-1340.

[10]

Elshamy, O.M., 2007. Experimental Investigations of Steady and Dynamic Behavior of Transverse Liquid Jets. University of Cincinnati, Cincinnati.

[11]

Gopala, Y., Zhang, P., Bibik, O., Lubarsky, E., Zinn, B., 2010. Liquid Fuel Jet in Crossflow -Trajectory Correlations Based on the Column Breakup Point. Paper Presented at the 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. https://doi.org/10.2514/6.2010-214.

[12]

He, Y., Yu, X., Wang, Z., Li, Z., Yan, Y., 2023. Numerical study on spray characteristics of kerosene jet in a crossflow. J. Propuls. Technol. 44 (3), 154-164. https://doi.org/10.13675/j.cnki.tjjs.210756.

[13]

Heister, S.D., Nguyen, T., Karagozian, A.R., 1989. Modeling of liquid jets injected transversely into a supersonic crossflow. AIAA J. 27 (12), 1727-1734. https://doi.org/10.2514/3.10327.

[14]

Hirt, C.W., Nichols, B.D., 1981. Volume of fluid (VOF) method for the dynamics of free boundaries. J. Comput. Phys. 39 (1), 201-225. https://doi.org/10.1016/0021-9991(81)90145-5.

[15]

Inamura, T., Nagai, N., 1997. Spray characteristics of liquid jet traversing subsonic airstreams. J. Propul. Power 13 (2), 250-256. https://doi.org/10.2514/2.5156.

[16]

Kong, X., He, W., Guo, Z., 2022. Investigation on spray characteristics of liquid jet in nonuniform crossflow. J. Aero. Power 37 (3), 534-544. https://doi.org/10.13224/j.cnki.jasp.20210151.

[17]

Li, C., Shen, C., Li, Q., Zhu, Y., 2019. Primary breakup process of liquid jet in supersonic crossflow. J. Natl. Univ. Def. Technol. 41 (4), 73-78.

[18]

Lin, S., Shen, C., Xiao, F., Zhu, Y., 2020. Large eddy simulation of primary breakup of transverse pulsed liquid jet in supersonic flow. J. Combust. Sci. Technol. 26 (1), 87-95.

[19]

Liu, N., 2015. Experimental Study And Large Eddy Simulation Of Primary Breakup Of Liquid Jet In Supersonic Cross Flow (Master). National University of Defense Technology Chang Sha (Available from: Cnki).

[20]

Liu, N., Wang, Z., Sun, M., Ralf, D., Wang, H., 2019. Simulation of liquid jet primary breakup in a supersonic crossflow under Adaptive Mesh Refinement framework. Aero. Sci. Technol. 91 (8), 456-473. https://doi.org/10.1016/j.ast.2019.05.017.

[21]

Menter, F.R., 1994. Two-equation eddy-viscosity turbulence models for engineering applications. AIAA J. 32 (8), 1598-1605. https://doi.org/10.2514/3.12149.

[22]

Olinger, D.S., Sallam, K.A., Lin, K.C., Carter, C.D., 2014. Digital holographic analysis of the near field of aerated-liquid jets in crossflow. J. Propul. Power 30 (6), 1636-1645. https://doi.org/10.2514/1.B34984.

[23]

Rachner, M., Becker, J., Hassa, C., Doerr, T., 2002. Modelling of the atomization of a plain liquid fuel jet in crossflow at gas turbine conditions. Aero. Sci. Technol. 6 (7), 495-506. https://doi.org/10.1016/S1270-9638(01)01135-X.

[24]

Rong, F., Jun, L., Yun, W., Jiajian, Z., Xiliang, S., Xipeng, L., 2018. Experimental investigation on Gliding arc discharge plasma ignition and flame stabilization in scramjet combustor. Aero. Sci. Technol. 79 (8), 145-153.

[25]

Schetz, J.A., Kush, E.A., Joshi, P.B., 1980. Wave phenomena in liquid jet breakup in a supersonic crossflow. AIAA J. 18 (7), 774-778. https://doi.org/10.2514/3.7687.

[26]

Shaolin, Wang, Huang, Y., Wang, F., Liu, Z., Liu, L., 2013. On the Breakup Process of Round Liquid Jets in Gaseous Crossflows at Low Weber Number. Paper Presented at the ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. https://doi.org/10.1115/GT2013-94696.

[27]

Tambe, S., 2004. Liquid Jets in Subsonic Crossflow. University of Cincinnati.

[28]

Tambe, S., Jeng, S.M., Mongia, H., Hsiao, G., 2005. Liquid Jets in Subsonic Crossflow. Paper Presented at the 43rd AIAA Aerospace Sciences Meeting and Exhibit. https://doi.org/10.2514/6.2005-731.

[29]

Wang, H., Kong, X., Guo, Z., 2023. Investigation on the trajectory and penetration of liquid jet in non-uniform crossflow. J. Aero. Power 38 (6), 1316-1327. https://doi.org/10.13224/j.cnki.jasp.20210552.

[30]

Wang, Q., Mondragon, U.M., Brown, C.T., McDonell, V.G., 2011. Characterization of trajectory, break point, and break point dynamics of A plain liquid jet in A crossflow. Atomization Sprays 21 (3), 203-219. https://doi.org/10.1615/AtomizSpr.2011002848.

[31]

Wang, Y., Yan, Y., Dang, L., Li, J., 2016. Numerical investigation on atomization characteristics of liquid jet in crossflow. J. Aero. Power 31 (10), 2464-2471. https://doi.org/10.13224/j.cnki.jasp.2016.10.020.

[32]

Wu, L., 2016. Breakup And Atomization Mechanism Of Liquid Jet In Supersonic Crossflows (Doctor). National University of Defense Technology Chang Sha (Available from: Cnki).

[33]

Wu, P.K., Kirkendall, K.A., Fuller, R.P., Nejad, A.S., 1997. Breakup processes of liquid jets in subsonic crossflows. J. Propul. Power 13 (1), 64-73. https://doi.org/10.2514/2.5151.

[34]

Yuan, C., 2018. Study on jet breakup in non-uniform air crossflow field. (Master), Civil Aviation University of China, Tian Jin (Available from: Cnki).

[35]

Zhang, B., Cheng, P., Li, Q., Chen, H., Li, C., 2021. Breakup process of liquid jet in gas film. Acta Phys. Sin. 70 (5), 230-241.

[36]

Zhang, J., Chang, J., Ma, J., Wang, Y., Bao, W., 2019. Investigations on flame liftoff characteristics in liquid-kerosene fueled supersonic combustor equipped with thin strut. Aero. Sci. Technol. 84 (1), 686-697.

[37]

Zhang, J., Chang, J., Ma, J., Zhang, C., Bao, W., 2017. Investigation of flame establishment and stabilization mechanism in a kerosene fueled supersonic combustor equipped with a thin strut. Aero. Sci. Technol. 70 (11), 152-160.

[38]

Zhang, J., Chang, J., Ma, J., Zhang, Y., Bao, W., 2018. Local and global flame characteristics in a liquid kerosene fueled supersonic combustor equipped with a thin strut. Aero. Sci. Technol. 76 (5), 49-57.

[39]

Zhu, Y., Huang, Y., Wang, F., Wang, X., 2010. Experiment on the breakup of round liquid jets in cross airflows. J. Aero. Power 25 (10), 2261-2266. https://doi.org/10.13224/j.cnki.jasp.2010.10.005.

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