Journal of Propulsion Technology ›› 2016, Vol. 37 ›› Issue (12): 2312-2319.

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Effects of Air-Cooled Ring Stabilizator Opening Angle

  

  1. School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,Beijing 100191,China,School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,Beijing 100191,China and School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,Beijing 100191,China
  • Published:2021-08-15

气冷环向稳定器张角对混合扩压器性能影响

刘友宏,周开福,牛俊杰   

  1. 北京航空航天大学 能源与动力工程学院,北京 100191,北京航空航天大学 能源与动力工程学院,北京 100191,北京航空航天大学 能源与动力工程学院,北京 100191
  • 作者简介:刘友宏,男,博士,教授,研究领域为传热传质、红外、力学等研究。

Abstract: In order to study the effects of air-cooled ring stabilizator opening angle on performance of the mixer and diffuser,for a new type of the mixer-diffuser and air-cooled stabilizator integration structure,the three-dimensional numerical simulation model based on the N-S equation was created. Through numerical simulation,the flow field,thermal mixing efficiency and flow loss of effect of different air-cooled ring stabilizator opening angles in the mixer and diffuser were obtained. The results show that,with the induction effect of air-cooled stabilizator,a large number of the fan cold flow invades the high temperature gas of the core flow,so that making a strong mixing between the core and fan flow and greatly improving the temperature of the fan cold flow. With the growing opening angle of air-cooled ring stabilizator,the stabilizator blockage ratio and flow loss increase,but the total-pressure recovery coefficient declines. The model with 14° opening angle has the highest total-pressure recovery coefficient of 0.992,and larger 0.002 than the minimum value. Therefore,the thermal mixing efficiency of the mixer and diffuser change little as the air-cooled ring stabilizator opening angle increases,and the difference between the maximum value and minimum value of thermal mixing efficiency is only 1.6% at the afterburner outlet.

Key words: The mixer and diffuser;Air-cooled ring stabilizator;Opening angle;Thermal mixing efficiency;Total-pressure recovery coefficient

摘要: 为了研究气冷环向稳定器张角对混合扩压器性能的影响规律,针对一种混合扩压器和气冷稳定器一体化新型结构,基于N-S方程建立了流场三维数值计算模型,采用数值模拟研究了气冷环向稳定器张角对混合扩压器流场、热混合效率和流动损失的影响规律。结果表明:在气冷稳定器的诱导作用下,外涵冷空气大量入侵内涵高温燃气,使内外涵流体之间进行强力掺混,大大提高了外涵冷空气温度;随着气冷环向稳定器张角的增大,稳定器堵塞比增大,流动损失增大,总压恢复系数减小;14°张角模型的混合扩压器总压恢复系数最大,其值为0.992,比最小值大0.002;此外,热混合效率随气冷环向稳定器张角的增加变化较小,加力燃烧室出口热混合效率最大值与最小值仅相差1.6%。

关键词: 混合扩压器;气冷环向稳定器;张角;热混合效率;总压恢复系数