中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Analysis of the Transonic Buffet Characteristics of Stationary and Pitching OAT15A Airfoil

文献类型:期刊论文

作者Nie, Xueyuan2,3; Zheng, Guannan2,3; Wei, Lianyi1,3; Huang, Chengde2,3; Yang, Guowei2,3; Ji, Zhanling2,3; Yang GW(杨国伟); Zheng GN(郑冠男); Nie XY(聂雪媛)
刊名APPLIED SCIENCES-BASEL
出版日期2024-08-01
卷号14期号:16页码:18
关键词transonic buffet shock wave DMD modes airfoil
DOI10.3390/app14167149
通讯作者Nie, Xueyuan(niexueyuan@imech.ac.cn) ; Zheng, Guannan(zhengguannan@imech.ac.cn)
英文摘要Transonic buffet flow is a classical complex and unstable flow that has a negative effect on aircraft fly safety. Therefore, it is crucial to study the unsteady characteristics of buffet flow. The numerical analysis method is very useful in achieving the aforementioned goal. In this paper, focused on the typical supercritical airfoil OAT15A in fixed and pitching conditions, unsteady Reynolds averaged Navier-Stokes (URANS) closed with the sst-k omega turbulence mode, coupled with the structure dynamical equation, is utilized to investigate the transonic buffet flow. Firstly, from the perspective of coherent flow structure, flow velocity divergence snapshots constructed from unsteady flow solutions are used to analyze the feature of transonic buffets in the two cases mentioned. Then, DMD modes are extracted by the dynamic mode decomposition technique from the velocity snapshots and adopted to analyze the flow modes of the two distinct flow fields. The numerical simulation results show that, in the fixed case, the regular motion feature of the buffet is present, the shock oscillation is closely related to the vortex structure, and the durations of rearward and forward movements of the shock are both equal to half of the buffet period. In the pitching case, the duration of the rearward motion of the primary shock is approximately five eighths of one buffet period, and the secondary shock appears with the primary one moving downstream, and they interact with each other. The region of the shock movement is larger than that of the fixed case, and there is chaotic flow rather than periodic flow in its wake. Structural elastic oscillation changes the characteristics of the aerodynamic response, which is solely affected by the frequency of the pitching oscillation.
WOS关键词FREQUENCY LOCK-IN
资助项目National Natural Science Foundation ; [12302230]
WOS研究方向Chemistry ; Engineering ; Materials Science ; Physics
语种英语
WOS记录号WOS:001305011800001
资助机构National Natural Science Foundation
源URL[http://dspace.imech.ac.cn/handle/311007/96496]  
专题力学研究所_流固耦合系统力学重点实验室(2012-)
通讯作者Nie, Xueyuan; Zheng, Guannan
作者单位1.Univ Chinese Acad Sci, Sch Future Technol, Beijing 100049, Peoples R China
2.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China
3.Chinese Acad Sci, Key Lab Mech Fluid Solid Coupling Syst, Inst Mech, Beijing 100190, Peoples R China
推荐引用方式
GB/T 7714
Nie, Xueyuan,Zheng, Guannan,Wei, Lianyi,et al. Analysis of the Transonic Buffet Characteristics of Stationary and Pitching OAT15A Airfoil[J]. APPLIED SCIENCES-BASEL,2024,14(16):18.
APA Nie, Xueyuan.,Zheng, Guannan.,Wei, Lianyi.,Huang, Chengde.,Yang, Guowei.,...&聂雪媛.(2024).Analysis of the Transonic Buffet Characteristics of Stationary and Pitching OAT15A Airfoil.APPLIED SCIENCES-BASEL,14(16),18.
MLA Nie, Xueyuan,et al."Analysis of the Transonic Buffet Characteristics of Stationary and Pitching OAT15A Airfoil".APPLIED SCIENCES-BASEL 14.16(2024):18.

入库方式: OAI收割

来源:力学研究所

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