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作 者:李世全 杨帆[1] 王宇辉 王健平[2] 张国庆[3] LI Shiquan;YANG Fan;WANG Yuhui;WANG Jianping;ZHANG Guoqing(College of Mechanical and Electrical Engineering,Beijing University of Chemical Technology,Beijing 100029,China;College of Engineering,Peking University,Beijing 100871,China;School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China)
机构地区:[1]北京化工大学机电工程学院,北京100029 [2]北京大学工学院,北京100871 [3]北京理工大学宇航学院,北京100081
出 处:《航空动力学报》2024年第5期80-94,共15页Journal of Aerospace Power
基 金:某装备发展部、装备预先研究领域基金(61407200113);国家自然科学基金(91741202,52076003);中央高校基本科研业务费专项资金(buctrc201913)。
摘 要:以铝粉为燃料,空气为氧化剂,通过一步反应机理,对不同当量比下气固两相旋转爆轰发动机的流场进行二维数值模拟研究。结果表明:由于颗粒注入速度和空气注入速度存在差异,导致反应物区中的颗粒三角区和空气三角区不完全重叠,使得当量比从0.6增加到1.4时,爆轰波前的平均局部当量比从0.929增加到2.093,爆轰波速度从2 070 m/s降低到1 690 m/s,爆轰波压力从5.67 MPa降低到4.87 MPa。燃烧室内基本的流场与气相旋转爆轰发动机相似,但气固两相之间的相互作用使得颗粒呈现出特有的分布特性,包括2个颗粒群和4条颗粒带以及它们之间的间隙。The flow field of a gas-solid two-phase rotating detonation engine taking aluminum powder as fuel and air as oxidant with one step reaction was investigated by two-dimensional numerical simulations at different equivalence ratios.Results showed that the velocity of the detonation wave decreased from 2070 m/s to 1690 m/s and detonation pressure decreased from 5.67 MPa to 4.87 MPa when the equivalence ratio increased from 0.6 to 1.4,because the average local equivalence ratio increased from 0.929 to 2.093,which was caused by incomplete overlapping of trigonal zones between air and particles because of the injection velocity difference between air and particles.The flow field was similar to that in gas phase rotating detonation engines.However,unique distribution characteristics,including two particle groups,four particle bands and gaps among them due to the interaction between gas phase and solid phase,were obtained.
分 类 号:V231.2[航空宇航科学与技术—航空宇航推进理论与工程]
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