施方成1,2, 高振勋1(), 田雨岩1, 蒋崇文1, 王田天2, 李椿萱1
收稿日期:
2021-08-23
修回日期:
2021-09-06
接受日期:
2021-11-03
出版日期:
2023-01-25
发布日期:
2021-11-10
通讯作者:
高振勋
E-mail:gaozhenxun@buaa.edu.cn
基金资助:
Fangcheng SHI1,2, Zhenxun GAO1(), Yuyan TIAN1, Chongwen JIANG1, Tiantian WANG2, Chun-Hian LEE1
Received:
2021-08-23
Revised:
2021-09-06
Accepted:
2021-11-03
Online:
2023-01-25
Published:
2021-11-10
Contact:
Zhenxun GAO
E-mail:gaozhenxun@buaa.edu.cn
Supported by:
摘要:
为探究亚格子模型和热效应对超声速喷流流场与声场的影响规律,采用LES/FW-H混合算法对超声速理想膨胀喷流开展了数值模拟参数研究。首先,通过对比数值模拟与实验数据详细验证了LES/FW-H混合算法的可靠性,并结合Tam相似谱理论确定了实验与数值模拟中声场出现偏差的原因在于实验中存在宽频激波噪声。之后,讨论了亚格子模型对流场平均量、湍流统计量和噪声特征的影响,数据对比表明动态Smagorinsky模型的模拟结果与隐式亚格子模型的结果一致,且均与已有实验和数值模拟结果相符;而采用常系数Smagorinsky模型将导致流场和声场结果出现明显偏差。最后,通过改变喷流出口总温研究了热效应对超声速理想膨胀喷流流场与声场的影响,研究发现喷流总温升高增大了无量纲的高频流向速度脉动,同时对远场高频噪声具有显著的增强效应。
中图分类号:
施方成, 高振勋, 田雨岩, 蒋崇文, 王田天, 李椿萱. 超声速理想膨胀喷流噪声的大涡模拟[J]. 航空学报, 2023, 44(2): 626266.
Fangcheng SHI, Zhenxun GAO, Yuyan TIAN, Chongwen JIANG, Tiantian WANG, Chun-Hian LEE. Large eddy simulation of ideally expanded supersonic jet noise[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626266.
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