零二次流引射器启动性能数值研究

推进技术 ›› 2010, Vol. 31 ›› Issue (2): 204-209.

零二次流引射器启动性能数值研究

许灵芝,徐旭

北京航空航天大学宇航学院;北京航空航天大学宇航学院

发布日期:2021-08-15
基金资助:
“九八五”工程资助项目(BHA985-2-1)

Numerical investigation on starting performance of zero-secondary flow ejectors

School of Astronautics,Beijing Univ. of Aeronautics and Astronautics,Beijing 100191,China;School of Astronautics,Beijing Univ. of Aeronautics and Astronautics,Beijing 100191,China

Published:2021-08-15

摘要/Abstract

摘要： 为研究零二次流引射器结构参数如何影响其启动性能,采用数值方法模拟求解了引射器流场,并分析了引射器从启动到不启动的典型工作状态。结果表明:扩压器入口面积与引射喷管喉部面积之比Ad/At和第二喉道收缩比Ast/Ad是影响引射器性能的首要因素,其次是第二喉道长径比Lst/Dst和第二喉道入口的位置Ld/Dd。Ad/At越大,扩压器入口斜激波越强,总压损失越大,临界启动压比越大,越难以启动;Ast/Ad越小(大于其临界收缩比)则临界启动压比越小,越易于启动。

关键词: 引射器+;引射喷管;结构参数;启动性能+,压力恢复,数值仿真

Abstract: To investigate how the geometry parameters can influence starting performance in zero-secondary flow ejector,flow field of different ejectors were solved by CFD. The numerical simulation results were also applied to analyze ejector typical operation modes,ranging from on-design to off-design point. Results suggest that Ad/A t (area ratio of diffuser entrance to nozzle throat) and A st /A d (second-throat contraction ratio) are the most important parameters on the ejector performance,and L st /D st (ratio of length to diameter second-throat) and Ld/D d (second-throat location) also greatly influence the performance. The critical starting pressure ratio is increased by increasing Ad/At. When A st /Ad is higher than second-throat critical contraction ratio,its decrease benefits starting the ejector.

Key words: Ejector+;Shrouded nozzle;Structure parameter;Starting performance+;Pressure recovery;Numerical simulation

许灵芝,徐旭. 零二次流引射器启动性能数值研究[J]. 推进技术, 2010, 31(2): 204-209.