航空学报2026，Vol.47Issue(17)：112-122,11.DOI:10.7527/S1000-6893.2026.32849
凹腔燃烧室中粉末燃料流动特性大涡模拟
Large eddy simulation on flow characteristics of powder fuel in a cavity combustor
摘要
Abstract
Based on the Large Eddy Simulation(LES)method,this paper provides a detailed investigation into the effects of powder fuel particle size,injection velocity,and incoming flow velocity on the powder fuel mixing characteris-tics within the combustion chamber of a scramjet.The study shows that smaller particles(2,5 μm)tend to flow near the wall and enter the cavity,while larger particles remain closer to the main flow region.The residence time of par-ticles in the cavity area(approximately 1 ms)is longer than that of particles outside the cavity(about 0.4 ms).For 2 μm and 5 μm particles,their trajectories cover the low-velocity recirculation zone inside the cavity,extending their residence time through a recirculation mechanism.At the same time,small particles(2,5 μm)induce significant fluc-tuations in the shear layer profile,and their motion is more easily influenced by the vortical structures of the flow field.The particle mass fraction reaches about 0.9 near the injection point but decreases rapidly downstream,dropping to approximately 0.1-0.3 in the main flow region.Increasing the injection velocity enhances the penetration depth of the particle jet,whereas raising the incoming flow Mach number reduces the particle residence time.Meanwhile,the in-creased momentum of the incoming flow makes it more difficult for the particle jet to penetrate the main flow region,re-sulting in noticeable jet deflection.This study provides a theoretical basis for the further design of powder fuel injection strategies.关键词
粉末燃料超燃冲压发动机/超声速流动/凹腔结构/颗粒喷射/掺混特性Key words
powder-fueled scramjet/supersonic flow/cavity structure/particle injection/mixing characteristics分类
航空航天引用本文复制引用
胡颖,董佳欣,王正阳,李超,任全彬..凹腔燃烧室中粉末燃料流动特性大涡模拟[J].航空学报,2026,47(17):112-122,11.基金项目
西北工业大学翱翔青年人才 Northwestern Polytechnical University Youth Talent Program （）
