带喉道注气的轴对称收扩喷管内流场计算研究
Computational analysis on internal performance of a convergent-divergent nozzle with throat fluidic injection
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摘要: 通过对带喉道注气控制的轴对称收扩喷管内流场计算研究,分析了喉道注气对喷管内流特性的影响.研究结果表明,相同落压比(NPR)下,随着二次流压比(SPR)的增大,喷管推力系数和流量系数均减小,其中对喷管推力系数的影响低于2%,而对喷管流量系数的影响可超过15%.并在此基础上,分别研究了喷管扩张比和调节片长度对喉道控制效果的影响,得到研究范围内相对较好的喷管计算模型.Abstract: The results of a computational study were presented to investigate the impact of throat fluidic injection on the flow field in an axisymmetric nozzle.With the increase of secondary pressure ratio(SPR),both the nozzle thrust ratio and mass flow ratio were reduced under the same nozzle pressure ratio(NPR).In addition,the effect of throat fluidic injection on the nozzle thrust ratio was less than 2%,but the effect on the nozzle mass flow ratio more than 15%.With the impact of the divergence ratio and adjustment sheet of the nozzle on the throat control effect presented,a better nozzle model was obtained within the scope of the investigation.
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Key words:
- throat area control /
- secondary flow /
- convergent-divergent nozzle /
- internal performance
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