IMECH-IR  > 非线性力学国家重点实验室
Acoustic Inversion for Uncertainty Reduction in Reynolds-Averaged Navier-Stokes-Based Jet Noise Prediction
Zhang XL(张鑫磊)1; Xiao, Heng2; Wu T(吴霆)1; He GW(何国威)1
Source PublicationAIAA JOURNAL
2022
Volume60Issue:7Pages:2407-2422
ISSN0001-1452
Abstract

The Reynolds-averaged Navier-Stokes (RANS)-based method is a practical tool to provide rapid assessment of jet noise-reduction concepts. However, the RANS-based method requires modeling assumptions to represent noise generation and propagation, which often reduces the predictive accuracy due to the model-form uncertainties. In this work, the ensemble Kalman filter-based acoustic inversion method is introduced to reduce uncertainties in the turbulent kinetic energy and dissipation rate based on the far-field noise and the axial centerline velocity data. The results show that jet noise data are more effective from which to infer turbulent kinetic energy and dissipation rate compared to velocity data. Moreover, the inferred noise source is able to improve the estimation of the turbulent flowfield and the far-field noise at unobserved locations. Further, the noise model parameters are also considered uncertain quantities, demonstrating the ability of the proposed framework to reduce uncertainties in both the RANS and noise models. Finally, one realistic case with experimental data is investigated to show the practicality of the proposed framework. The method opens up the possibility for the inverse modeling of jet noise sources by incorporating far-field noise data that are relatively straightforward to be measured compared to the velocity field.

DOI10.2514/1.J060876
Indexed BySCI ; EI
Language英语
WOS IDWOS:000742546900001
WOS KeywordDATA ASSIMILATION ; MIXING NOISE ; MEAN-FLOW ; OPTIMIZATION ; ANALOGY ; SPACE ; MODEL ; SPEED
WOS Research AreaEngineering
WOS SubjectEngineering, Aerospace
Funding ProjectNational Science Foundation of China Basic Science Center Program for Multiscale Problems in Nonlinear Mechanics[11988102] ; Strategic Priority Research Program of the Chinese Academy of Sciences[XDB22040104] ; Key Research Program of Frontier Sciences of the Chinese Academy of Sciences[QYZDJ-SSWSYS002]
Funding OrganizationNational Science Foundation of China Basic Science Center Program for Multiscale Problems in Nonlinear Mechanics ; Strategic Priority Research Program of the Chinese Academy of Sciences ; Key Research Program of Frontier Sciences of the Chinese Academy of Sciences
Classification一类/力学重要期刊
Ranking1
Citation statistics
Cited Times:3[WOS]   [WOS Record]     [Related Records in WOS]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/88376
Collection非线性力学国家重点实验室
Corresponding AuthorHe GW(何国威)
Affiliation1.Chinese Acad Sci, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China
2.Virginia Tech, Kevin T Crofton Dept Aerosp & Ocean Engn, Blacksburg, VA 24060 USA
Recommended Citation
GB/T 7714
Zhang XL,Xiao, Heng,Wu T,et al. Acoustic Inversion for Uncertainty Reduction in Reynolds-Averaged Navier-Stokes-Based Jet Noise Prediction[J]. AIAA JOURNAL,2022,60,7,:2407-2422.
APA Zhang XL,Xiao, Heng,Wu T,&He GW.(2022).Acoustic Inversion for Uncertainty Reduction in Reynolds-Averaged Navier-Stokes-Based Jet Noise Prediction.AIAA JOURNAL,60(7),2407-2422.
MLA Zhang XL,et al."Acoustic Inversion for Uncertainty Reduction in Reynolds-Averaged Navier-Stokes-Based Jet Noise Prediction".AIAA JOURNAL 60.7(2022):2407-2422.
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