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多喷嘴引射器性能计算模型 被引量:7
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作者 邱义芬 王俊清 +1 位作者 袁修干 韩凤华 《北京航空航天大学学报》 EI CAS CSCD 北大核心 1997年第5期621-626,共6页
本文对多喷嘴引射器的工作过程进行分析,给出了引射器性能参数的理论计算方法,得出影响引射器性能的因素.经试验验证该计算方法有较高的精度,为引射器的设计提供了理论依据.
关键词 超临界 引射器 喷嘴飞机 环境控制系统
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Numerical simulations of buoyant reactive jets with sidewall effects 被引量:2
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作者 ZHANGHeping JIANGXi +3 位作者 WANGWei YANGYun XULiang FANWeicheng 《Chinese Science Bulletin》 SCIE EI CAS 2004年第19期2105-2109,共5页
The near field dynamics of buoyant reactive jets with adjacent sidewalls is investigated by time-dependent three-dimensional direct simulations. The physical problem is a fuel jet issuing vertically into an oxidant am... The near field dynamics of buoyant reactive jets with adjacent sidewalls is investigated by time-dependent three-dimensional direct simulations. The physical problem is a fuel jet issuing vertically into an oxidant ambient envi- ronment in a corner configuration with sidewall boundaries. Simulation results are presented for two cases with different jet nozzle geometries: a corner-round reactive jet and a cor- ner-square reactive jet with the same cross-sectional area on the nozzle plane. Buoyancy-induced large vortical structures evolve spatially in the flow field and transition to turbulence occurs downstream. Calculation of the mean flow properties shows that entrainment of the corner-round jet is stronger than that of the corner-square jet due to the stronger vortex deformation in the corner-round case. 展开更多
关键词 数字模拟 浮力作用喷气式发动机 雾沫夹带 喷嘴飞机 燃油喷射
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