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二元高超声速进气道内压缩通道/隔离段曲面构型 被引量:11
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作者 张晓嘉 梁德旺 黄国平 《推进技术》 EI CAS CSCD 北大核心 2008年第1期49-53,共5页
对于二元高超声速进气道内压缩通道及隔离段设计,提出了进气道下壁弧形曲面构型方案。在一系列不同收缩比、不同波系配置的平面构型进气道基础上,通过基于N-S方程的数值模拟研究了不同半径的弧形过渡曲面对进气道性能的影响。发现采用... 对于二元高超声速进气道内压缩通道及隔离段设计,提出了进气道下壁弧形曲面构型方案。在一系列不同收缩比、不同波系配置的平面构型进气道基础上,通过基于N-S方程的数值模拟研究了不同半径的弧形过渡曲面对进气道性能的影响。发现采用弧形曲面过渡可以削弱平面构型方案对气流不必要的膨胀,减小隔离段进口处上侧壁面高压,改善隔离段进口气流均匀性。新构型有助于降低起动马赫数,且弧形过渡半径越大,收缩比越大,降低的程度越明显;还可以大大提高进气道的总压恢复,无须最后一道内压激波打在下壁面肩点上即可获得较高的性能。 展开更多
关键词 高超声速进气道 数值仿真 内压式进气道 隔离器 曲面 构型
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ANALYSIS OF INTERNAL WAVERIDER INLET AND TYPICAL SIDEWALL COMPRESSION INLET PERFORMANCE 被引量:4
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作者 黄国平 朱呈祥 +1 位作者 尤延铖 周淼 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2011年第1期120-128,共9页
A new internal waverider inlet with a rectangular shape of entrance and exit in front view is designed at Ma=6.0.The design is based on a better basic flowfield ICFC than traditional one and derived with the technolog... A new internal waverider inlet with a rectangular shape of entrance and exit in front view is designed at Ma=6.0.The design is based on a better basic flowfield ICFC than traditional one and derived with the technology of stream tracing and shock cutting.Comparison between the newly designed inlet and a typical sidewall compression inlet is given.The design Mach number and entrance shape of this new inlet are chosen according to the sidewall compression inlet.Numerical results show that most of the performance parameters of the internal waverider inlet are a bit higher than the sidewall inlet,such as the flow capture coefficient,total pressure recovery and the kinetic efficiency.The performances of these two inlets at off-design points are compared.The internal waverider inlet can capture more than 91% of incoming flow under all simulated conditions.Results show that internal waverider inlet using 3-D compression and high flow capture coefficient is a kind of fixed-geometry inlet with better performance. 展开更多
关键词 HYPERSONIC PERFORMANCE internal waverider inlet sidewall compression inlet
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