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基于引射器函数法的程序优化设计及验证
引用本文:查柏林,李思冶,权辉,王金金.基于引射器函数法的程序优化设计及验证[J].航空动力学报,2021,36(6):1324-1334.
作者姓名:查柏林  李思冶  权辉  王金金
作者单位:1.火箭军工程大学 导弹工程学院,西安 710025
基金项目:国家自然科学基金(52003296); 陕西省自然科学基础研究计划(2020JQ-488)
摘    要:针对考虑多因素综合影响的引射器优化问题,基于引射器函数法,深入研究了静压协调函数的数学特性并分析了其数学曲线上的奇异点。在此基础上,通过程序设计和基准推进归纳法得到了多分支工作特性曲线,分析了不同分支下解的特性。另外结合工作特性曲线重点研究了混合室背压、主次流总压比和混合不均匀度对引射性能的影响,提出了静压特性曲面、临界曲线的设计概念。通过试验数据对比分析验证了引射器函数法的可靠性。结论表明:靠近临界曲线工况时引射器设计性能较好;混合不均匀度对引射性能影响重大,不均匀度为1.5时对比理想状态,引射系数最大误差达到32.73%;考虑壁面摩擦设计时需对摩擦因数公式模型进行修正。研究结果为引射器优化设计提供了重要指导。 

关 键 词:引射器函数法    静压协调函数    程序优化设计    多分支工作特性曲线    静压特性曲面
收稿时间:2020/9/18 0:00:00

Program optimization design and verification based on ejector function method
ZHA Bolin,LI Siye,QUAN Hui,WANG Jinjin.Program optimization design and verification based on ejector function method[J].Journal of Aerospace Power,2021,36(6):1324-1334.
Authors:ZHA Bolin  LI Siye  QUAN Hui  WANG Jinjin
Institution:1.School of Missile Engineering,Rocket Force University of Engineering,Xi’an 710025,China2.Project Management Center,Equipment Department of Rocket Force,the Chinese People’s Liberation Army,Beijing 100085,China
Abstract:In view of the ejector optimization problem considering the comprehensive influence of multiple factors, based on the ejector function method, the mathematical characteristics of static pressure matching function were studied and the singular points on the mathematical curve were analyzed. On this basis, the multi branch characteristic curves were obtained by programming and benchmark progression induction method, and the characteristics of solutions under different branches were analyzed. In addition, the influences of mixing chamber back pressure, total pressure ratio of primary and secondary flow and mixing nonuniformity on the ejector performance were studied, and the design concepts of static pressure characteristic curve and critical curve were proposed. The reliability of the ejector function method was verified by comparing with the experimental data. The results showed that the design performance of the ejector was better when it was close to the critical curve. The mixing nonuniformity had a great influence on the ejector performance, when the nonuniformity was 1.5, compared with the ideal state, the maximum error of the ejecting coefficient reached 32.73%. When considering the wall friction design, the friction coefficient formula model should be modified. The results provide an important guidance for the optimal design of ejector.
Keywords:ejector function method  static pressure matching function  program optimization design  multi branch working characteristic curve  static pressure characteristic surface
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