Journal of Propulsion Technology ›› 2015, Vol. 36 ›› Issue (8): 1215-1221.

• Combustion , Heat and Mass Transfer • Previous Articles     Next Articles

Computational Model of Rotating Orifice

  

  1. School of Power and Energy,Northwestern Polytechnical University,Xi’an 710072,China,School of Power and Energy,Northwestern Polytechnical University,Xi’an 710072,China and School of Power and Energy,Northwestern Polytechnical University,Xi’an 710072,China
  • Published:2021-08-15

考虑入射角影响的旋转孔计算模型

朱鹏飞,刘振侠,吕亚国   

  1. 西北工业大学 动力与能源学院,陕西 西安 710072,西北工业大学 动力与能源学院,陕西 西安 710072,西北工业大学 动力与能源学院,陕西 西安 710072
  • 作者简介:朱鹏飞(1988—),男,博士生,研究领域为航空发动机润滑系统与空气系统。

Abstract: In order to analyze the flow characteristics of rotating orifice,and improve the efficiency of air system one-dimensional simulation,the computational model of rotating orifice was developed considering the main factors,such as,incidence angle,geometric parameters. The simulation model was constructed based on MATLAB/Simulink. The model was verified by experimental data and commercial software Flowmaster. The results show that error between the model and experimental results is within 7.2%,and error between the model and CFD results does not exceed 2.3%. However,error between the model and Flowmaster results is close to 8.94%. The results show that model of rotating orifice has high precision,and can be applied to simulate different type of axial orifices,which is of great significance for air system one-dimensional simulation.

Key words: Air system;Rotating orifice;Incidence angle;Discharge coefficient

摘要: 为分析旋转孔的流动特性,提高空气系统一维仿真计算效率,综合考虑入射角、几何参数等主要影响因素,建立了旋转孔流动特性计算模型,并利用MATLAB/Simulink软件搭建其仿真模型。通过试验结果和商业软件Flowmaster对该模型进行验证,结果表明:该模型计算结果与试验结果误差在7.2%内,与CFD数值计算结果的最大误差不超过2.3%,而Flowmaster计算结果与试验结果最大误差达到8.94%。旋转孔模型计算结果准确度高,适用于不同类型轴向孔的模拟。

关键词: 空气系统;旋转孔;入射角;流量系数