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侧压式进气道内部阻力分析
引用本文:骆晓臣,张堃元.侧压式进气道内部阻力分析[J].推进技术,2007,28(2):204-207.
作者姓名:骆晓臣  张堃元
作者单位:南京航空航天大学,能源与动力学院,江苏,南京,210016
基金项目:国家高技术研究发展计划(863计划)
摘    要:针对目前对超燃冲压发动机阻力特性的需要,以侧压式进气道为例,分别以内壁面和捕获流管为分析体,对其内部阻力进行分类;以数值模拟为手段,给出了总阻力的大小及各项阻力的分配比例,并分析了进气道几何参数变化对阻力的影响关系。

关 键 词:侧压式进气道  摩擦阻力  压力阻力  附加阻力  阻力分配
文章编号:1001-4055(2007)02-0204-04
收稿时间:2006-01-19
修稿时间:2006-06-26

Analysis for internal drag in sidewall-compression inlet
LUO Xiao-chen,ZHANG Kun-yuan.Analysis for internal drag in sidewall-compression inlet[J].Journal of Propulsion Technology,2007,28(2):204-207.
Authors:LUO Xiao-chen  ZHANG Kun-yuan
Institution:Coll. of Energy and Power, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:The classification of the internal drags on sidewall-compression inlets was presented for the requirement of drag characters on scramjet.The walls inside of the inlet and captured flow tubes were used respectively to analyze drags.The total drag and component of different internal drag were given through numerical investigation.The influence of inlet configurations to the internal drag was discussed.
Keywords:Sidewall-compression inlet  Friction drag  Pressure drag  Additive drag  Drag distribution
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