Review of atomization mechanism and spray characteristics of a liquid jet in supersonic crossflow  

作　　者：Yaozhi ZHOU Zun CAI Qinglian LI Chenyang LI Mingbo SUN Peibo LI Hongbo WANG 

机构地区：[1]College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China [2]Beijing Institute of Tracking and Telecommunication Technology,Beijing 100094,China

出　　处：《Chinese Journal of Aeronautics》2023年第8期1-23,共23页中国航空学报（英文版）

基　　金：supports from the National Natural Science Foundation of China(Nos.11902353,12272408,12102472,11902351,and 12102462);the National Science Fund for Distinguished Young Scholars,China(No.11925207);the Hunan Provincial Postgraduate Research Innovation Project,China(No.CX20210035).

摘　　要：The injection and atomization process of a liquid fuel jet is critical for an ignition start of a scramjet engine.Airwall-mounted crossflow injection strategy is widely used in scramjet combustors,avoiding high total pressure loss and allowing the liquid fuel to rapidly undergo atomization,mixing,and evaporation.In this review,research progress on a liquid jet in supersonic crossflow was evaluated from aspects of atomization mechanism and spray characteristics.When a liquid jet is injected into a supersonic crossflow,primary and secondary breakups occur successively.The surface instability of liquid can significantly affect the breakup process.This review discusses the current understanding of the breakup process and spray characteristics of a liquid jet in supersonic crossflow including the mechanism of atomization and the characteristics of distribution and atomization.The development of windward Rayleigh-Taylor(R-T)unstable waves is the main factor in column breakup.The development of Kelvin-Helmholtz(K-H)unstable waves along the circumferential direction of the jet or droplets is the main factor of surface and droplet breakups.The liquid-gas momentum ratio is the most important factor affecting the penetration depth.The span width of the liquid jet is affected by the windward area.Breakup and coalescence lead to a transformation of the size distribution of droplets from S-or C-shaped to I-shaped,and the velocity distribution of the droplets on the central symmetry plane has a mirrored S-shape.The droplet distribution on the spanwise cross-section retains a structure similar to an“Ω”shape.At last,some promising recommendations have been proposed,namely a theoretical predictive model which can describe the breakup mechanism of a liquid jet,the distribution characteristics and droplets size distribution of a liquid jet under a cavity combustion chamber,especially for enthalpy flows with complex wave structures.

关 键 词：ATOMIZATION Liquid fuels Spraynozzles Supersonicflow Two phase flow 

分 类 号：V235.21[航空宇航科学与技术—航空宇航推进理论与工程]