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基于紊动射流理论的变循环压缩系统降维数值研究

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模式选择阀门是变循环压缩系统模式转换过程中实现参数可调的重要部件,在进行压缩系统性能分析时,高计算效率和计算精度的平衡是研究人员关注的重要内容.本文建立了基于紊动射流理论的降维数值方法,并将其运用于变循环压缩系统数值仿真中,将计算结果与现有的突扩型降维数值方法和全三维模式选择阀门数值方法的计算结果进行对比分析.研究表明:基于紊动射流理论的降维数值方法可以更加准确地预测阀门的压力损失,相比于突扩降维模型平均误差由19.41%下降到5.60%.在小开度下,基于紊动射流理论的降维数值方法可以更加准确地得到前风扇部件在模式转换过程中的总压比和涵道比变化规律,总压比的预测误差由1.07%下降为0.15%,涵道比的预测误差由32.38%下降为3.50%;大开度工况下,所发展的新型降维数值方法与现有的突扩型降维数值方法精度相当.但基于紊动射流理论的降维数值方法通过将模式选择阀门上下游涵道内气动参数相互关联,获得相对准确的模式选择阀门下游速度分布,是一种可用于变循环压缩系统数值模拟的降维方法.
Numerical study on dimension reduction of variable cycle compression system based on turbulent jet theory
The mode selection valve is an important component to change thermodynamic cycle parameters in the mode transition process of the variable cycle compression system.In the performance analysis of the com-pression system,the balance between high computational efficiency and computational accuracy is an important part of the researchers'attention.In this paper,a reduced-dimensional numerical method based on turbulent jet theory is established and applied to the numerical simulation of variable cycle compression system.The calcula-tion results are compared with the sudden expansion reduced-dimensional numerical method and the full three-dimensional mode selection valve numerical method.The results show that:the reduced-dimensional numerical method based on the turbulent jet theory can predict the pressure loss of the valve more accurately.Compared with the sudden expansion reduced-dimensional numerical method,the average error decreases from 19.41%to 5.60%.At the small opening,the reduced-dimensional numerical method based on the turbulent jet theory can more accurately obtain the total pressure ratio and the bypass ratio of the front fan during the mode transition pro-cess.The prediction error of the total pressure ratio decreases from 1.07%to 0.15%,and the prediction error of the bypass ratio decreases from 32.38%to 3.50%.At the large opening,the accuracy of the new reduced-dimen-sional numerical method is equivalent to the sudden expansion reduced-dimensional numerical method.By corre-lating the upstream and downstream aerodynamic parameters of the mode selection valve in the bypass,a relative-ly accurate downstream velocity distribution of the mode selection valve is obtained,so the new method based on the turbulent jet theory can be used for the numerical simulation of the variable cycle compression system.

Variable cycle engineVariable cycle compression systemMode selection valveTurbu-lent jetReduced-dimensional numerical method

梁熙文、王掩刚、吴桐、王昊

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西北工业大学 动力与能源学院,陕西 西安 710072

变循环发动机 变循环压缩系统 模式选择阀门 紊动射流 降维数值方法

2025

推进技术
航天科工集团公司三十一研究所

推进技术

北大核心
影响因子:0.631
ISSN:1001-4055
年,卷(期):2025.46(1)