环簇式塞式喷管中立体激波的拓扑结构
Topological structure of stereo shocks in the annular clustered plug nozzle
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摘要: 采用仅显示环簇式塞式喷管单元间干涉激波区域网格点作为可视化方法对数值模拟结果进行后处理,得到了直观的三维干涉激波图像,并归纳得到三种干涉激波的拓扑结构和一种脊状能量泄漏区.结合文献中的实验数据分析了三种拓扑结构所造成的干涉损失,为设计提供参考.Abstract: By using a visualization method which only shows the grids of the stereo shock zones between unites of the annular clustered plug nozzle,the numerical results were reprocessed.From the visualized images of the three-dimension interference shock,three kinds of topological structures of interference shock and a kind of ridge contour of energy leak were summarized.The performance loss caused by these three topological structures was analyzed with the aid of the experimental data,thus providing a reference for further design.
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Key words:
- topological structure /
- shock /
- plug nozzle /
- rocket engine
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