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出口宽高比及旋流角对双涵道S弯喷管温度分布的影响

孙鹏 周莉 王占学 史经纬

孙鹏, 周莉, 王占学, 史经纬. 出口宽高比及旋流角对双涵道S弯喷管温度分布的影响[J]. 航空动力学报, 2022, 37(2): 391-403. doi: 10.13224/j.cnki.jasp.20210149
引用本文: 孙鹏, 周莉, 王占学, 史经纬. 出口宽高比及旋流角对双涵道S弯喷管温度分布的影响[J]. 航空动力学报, 2022, 37(2): 391-403. doi: 10.13224/j.cnki.jasp.20210149
SUN Peng, ZHOU Li, WANG Zhanxue, SHI Jingwei. Effect of aspect ratio and swirl angle on temperature distribution of double serpentine nozzle for turbofan[J]. Journal of Aerospace Power, 2022, 37(2): 391-403. doi: 10.13224/j.cnki.jasp.20210149
Citation: SUN Peng, ZHOU Li, WANG Zhanxue, SHI Jingwei. Effect of aspect ratio and swirl angle on temperature distribution of double serpentine nozzle for turbofan[J]. Journal of Aerospace Power, 2022, 37(2): 391-403. doi: 10.13224/j.cnki.jasp.20210149

出口宽高比及旋流角对双涵道S弯喷管温度分布的影响

doi: 10.13224/j.cnki.jasp.20210149
基金项目: 国家自然科学基金(51876176,52076180,51906204); 国家科技重大专项(J2019-Ⅱ-0015-0036);陕西省杰出青年基金(2021JC-10)
详细信息
    作者简介:

    孙鹏(1991-),男,博士生,主要从事S弯异形喷管流动及气动变形方面的研究。

    通讯作者:

    周莉(1978-),女,教授、博士生导师,博士,研究领域为排气系统设计及流动控制技术。E-mail:zhouli@nwpu.edu.cn

  • 中图分类号: V231.1

Effect of aspect ratio and swirl angle on temperature distribution of double serpentine nozzle for turbofan

  • 摘要: 采用数值方法研究了出口宽高比及旋流角对基于真实排气混合器构型的双涵道S弯喷管内/外流场温度分布的影响。结果显示:在圆转方弯曲构型的作用下,波瓣混合器及尾锥诱导产生的流向涡在第二弯通道及等直段内部卷吸着热流冲击S弯喷管壁面形成“热斑”。在完全遮挡高温部件准则的约束下,随着出口宽高比的增加,S弯喷管壁面的“热斑”温度先增大后减小,当出口宽高比为5时,壁面“热斑”温度最高,相比喷管基准模型增加1.3%。而出口宽高比的增加导致喷管出口下游尾焰的长度逐渐缩短。随着旋流角的增加,喷管下壁面的“热斑”温度先减小后增大,旋流角为10°时达到最小值,壁面温度峰值相比无旋流角工况降低15.9%。而旋流角增加导致喷管出口下游尾焰的宽度逐渐增大,长度逐渐缩短。

     

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出版历程
  • 收稿日期:  2021-04-06
  • 刊出日期:  2022-02-28

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