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Evolution of weakly unstable oblique detonation in disturbed inflow
Niu, Shuzhen1; Yang PF(杨鹏飞)2; Xi, Xuechen1,3; Li, Zhenzhen1; Teng, Honghui1,4
Corresponding AuthorLi, Zhenzhen([email protected]) ; Teng, Honghui([email protected])
Source PublicationPHYSICS OF FLUIDS
2024
Volume36Issue:1Pages:12
ISSN1070-6631
AbstractThe surface instability of oblique detonation waves (ODWs) without perturbations has been extensively investigated, yet the impact of external perturbations remains under-explored. Utilizing reactive Euler equations coupled with a two-step induction-exothermic reaction model, this study conducts a numerical examination of the evolution of unstable ODW surfaces subjected to a continuous sinusoidal density/temperature perturbation inflow. The results show that, without inflow perturbations, the ODW can evolve into triple points in the downstream due to detonation instability, similar to previous work. However, a small continuous perturbation can induce a significant forward movement of the ODW unstable position. Surprisingly, as the perturbation magnitude increases, the changes in the unstable position become progressively less pronounced. By increasing the perturbation frequency, the oscillation amplitude first increases, but a decreasing period/stage occurs with a modest frequency. To investigate the response of ODW to the increase in perturbation, the frequency characteristics and numerical smoked cells of detonation surfaces are examined and analyzed using Fast Fourier Transformation. The power spectral density indicates the presence of two distinct oscillation modes within oblique detonation. Low-frequency, small-amplitude perturbations serve to amplify the instability of the detonation, and more irregular oscillations could be observed. Conversely, high-frequency, large-amplitude perturbations suppress the development of small-scale waves on the detonation wavefront and lead to a relative regular oscillation, indicating that the wavefront pressure oscillations are entirely determined by inflow perturbations and become predictable. These findings have significant implications for the control of intrinsically unstable ODWs, providing valuable insights into the regulation of ODW dynamics.
DOI10.1063/5.0184971
Indexed BySCI ; EI
Language英语
WOS IDWOS:001138760800016
WOS KeywordNUMERICAL-SIMULATION ; CELLULAR STRUCTURE ; WAVES ; WEDGE ; PROPAGATION ; INSTABILITY ; MECHANISMS ; INITIATION ; STEADY
WOS Research AreaMechanics ; Physics
WOS SubjectMechanics ; Physics, Fluids & Plasmas
Classification一类/力学重要期刊
Ranking2
ContributorLi, Zhenzhen ; Teng, Honghui
Citation statistics
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/94647
Collection高温气体动力学国家重点实验室
Affiliation1.Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China;
2.Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China;
3.Shanxi Police Coll, Dept Publ Secur, Taiyuan 030401, Shanxi, Peoples R China;
4.Aero Engine Acad China, Adv Jet Prop Innovat Ctr, Beijing 101300, Peoples R China
Recommended Citation
GB/T 7714
Niu, Shuzhen,Yang PF,Xi, Xuechen,et al. Evolution of weakly unstable oblique detonation in disturbed inflow[J]. PHYSICS OF FLUIDS,2024,36,1,:12.Rp_Au:Li, Zhenzhen, Teng, Honghui
APA Niu, Shuzhen,杨鹏飞,Xi, Xuechen,Li, Zhenzhen,&Teng, Honghui.(2024).Evolution of weakly unstable oblique detonation in disturbed inflow.PHYSICS OF FLUIDS,36(1),12.
MLA Niu, Shuzhen,et al."Evolution of weakly unstable oblique detonation in disturbed inflow".PHYSICS OF FLUIDS 36.1(2024):12.
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