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超燃冲压发动机各部件阻力特性仿真分析

Simulation and Analysis of Internal Drag Characteristics for Different Components of Scramjet
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摘要 采用CFD技术,对高超声速冲压发动机冷流状态下阻力特性开展了数值模拟研究。对发动机不同部件的阻力大小及不同阻力类型的占比进行了对比分析,为发动机性能预测和评估提供了有效支撑。 Using CFD technology,a numerical simulation study was conducted on internal drag characteristics of scramjet under cold flow conditions.The drag of different parts of the engine and the proportion of different drag types were compared and analyzed,which provides effective support for engine performance prediction and evaluation.
作者 潘沙 李佳豪 尹丹 唐旭荣 帅政阳 吴辉 PAN Sha;LI Jia-hao;YIN Dan;TANG Xu-rong;SHUAI Zheng-yang;WU Hui(Academy of Hi-Tech Research,Hunan Institute of Traffic Engineering,Hengyang 421009,China;School of Mechanical and Electrical Engineering,Hunan Institute of Traffic Engineering,Hengyang 421009,China)
出处 《内燃机与配件》 2021年第10期44-45,共2页 Internal Combustion Engine & Parts
关键词 高超声速 超燃冲压发动机 阻力 数值模拟 计算流体力学 hypersonic scramjet drag numerical simulation computational fluid dynamics
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  • 1[1]刘兴州.飞航导弹动力装置[M].北京:宇航出版社,1992.
  • 2[2]Menon S, Seitzman J.Mixing and Combustion in Scramjet Combustors[R].AIAA2004-3826.
  • 3[3]Yu G.Investigation of Fuel Injection and Flame Stabilization in Liquid Hydrocarbon-Fueled Supersonic Combustors[R].AIAA2001-3608.

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