考虑侧壁效应的遮檐式空腔流声耦合特性研究

doi:10.7527/S1000-6893.2026.34094

Abstract

Abstract: Overhanging lip cavity flow widely exists in engineering, but the influence mechanism of the side wall of the finite-width overhanging lip cavity on the flow evolution and fluctuating pressure characteristics is not clear. In this paper, combined with wind tunnel test and detached eddy simulation ( DES ), the influence of the side wall on the spatial distribution and power spectral density characteristics of the fluctuating pressure energy of the overhanging lip cavity under the wind speed of 40 m/s-70 m / s is studied, and the flow-acoustic coupling mechanism of the overhanging lip cavity is analyzed simultaneously. The results show that the spatial distribution of fluctuating pressure energy is dispersed at low wind speed, and the contribution of near-wall region is obvious. As the wind speed increases, the low-frequency energy gradually concentrates to the middle of the cavity. The power spectral density of fluctuating pressure in the central section shows a significant narrow-band peak at 300-450 Hz. The peak frequency increases with the increase of wind speed, and the growth rate slows down at high wind speed. High-frequency characteristic peaks of 1220-1240 Hz appear at the measuring points on the side wall. Affected by the side wall surface, the vortex structure near the cavity wall is broken into small-scale vortices, which induces high-frequency fluctuating pressure on the side wall surface. The self-sustaining oscillation of the cavity and the acoustic mode have flow-acoustic coupling, which excites the high-frequency discrete peak of the fluctuating pressure. It provides a theoretical basis for the design and oscillation suppression of a finite-width overhanging lip cavity.

Key words: overhanging lip cavity, sidewall effect, detached eddy simulation, flow-acoustic coupling, wind-tunnels

CLC Number:

V211.3

References

[1] RICCIARDI T R, WOLF W R, MOFFITT N J, et al. Numerical noise prediction and source identification of a realistic landing gear [J]. Journal of Sound and Vibration, 2021, 496: 115933. [2] NERI E, KENNEDY J, BENNETT G J. Bay cavity noise for full-scale nose landing gear: A comparison between experimental and numerical results [J]. Aerospace science and technology, 2018, 72: 278-291. [3] CARROLL D, POTT-POLENSKE M, BENNETT G J. Air curtains for landing gear noise reduction [J]. Aerospace science and technology, 2025, 161: 110139. [4] 郑国雨, 孙一峰, 张亦知, 等. 基于导流板的前起落架舱空腔噪声抑制研究 [J]. 振动与冲击, 2024, 43(19): 145-152. ZHENG G Y, SUN Y F, ZHANG Y Z,et al. Noise suppression of front landing gear cabin cavity based on deflectors [J]. Journal of Vibration and Shock, 2024, 43(19): 145-152. [5] HE Y, THOMPSON D, HU Z. Aerodynamic noise from a high-speed train bogie with complex geometry under a leading car [J]. Journal of Wind Engineering and Industrial Aerodynamics, 2024, 244: 105617. [6] KIM H, HU Z, THOMPSON D. Effect of cavity flow control on high-speed train pantograph and roof aerodynamic noise [J]. Railway Engineering Science, 2020, 28(1): 54-74. [7] ZHU L, WU T, HE G. Large-eddy simulation for the aero-vibro-acoustic analysis: plate-cavity system excited by turbulent channel flow [J]. Acta Mechanica Sinica, 2022, 38(10): 1-18. [8] 漆琼芳, 邓海华, 苗天丞, 等. 船模水动力噪声及孔腔激励载荷试验与计算对比分析 [J]. 振动与冲击, 2024, 43(15): 288-93+310. QI Q F, DENG H H, MIAO T C, et al. Comparative analysis of ship model hydrodynamic noise and hole cavity excitation load tests and calculation [J]. Journal of Vibration and Shock, 2024, 43(15): 288-93+310. [9] 张志飞, 任辉, 曹斯诗, 等. 平面射流的汽车天窗风振降噪特性 [J]. 振动与冲击, 2023, 42(03): 209-216. ZHANG Z F, REN H, CAO S S, et al. Buffeting noise reduction characteristics of vehicle sunroof with plane jet [J]. Journal of Vibration and Shock, 2023, 42(03): 209-216. [10] ROSSITER J. Wind-tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds [R]. London, 1964. [11] CROOK S D, LAU T C W, KELSO R M. Three-dimensional flow within shallow, narrow cavities [J]. Journal of Fluid Mechanics, 2013, 735: 587-612. [12] GUO G, GONG J, ZHANG M. Numerical investigation on flow characteristics of low-speed flow over a cavity with small aspect ratio [J]. International Journal of Mechanical Sciences, 2020, 178. [13] ZHANG K, NAGUIB A M. Effect of finite cavity width on flow oscillation in a low-Mach-number cavity flow [J]. Experiments in fluids, 2011, 51(5): 1209-1229. [14] XU J, LEI J, WU J, et al. The three-dimensional characteristics of the unsteady wall-pressure in a low-Mach-number rectangular cavity flow with Rossiter model oscillation [J]. Experiments in fluids, 2017, 58(9): 109. [15] KIM T U, PARK S H, LEE S, et al. Analysis of Flow Oscillation Due to Sidewall of Three-Dimensional Supersonic Open Cavity Flow [J]. International Journal of Aeronautical and Space Sciences, 2019, 20(4): 839-849. [16] HUANG Y-X, CHUNG K-M. Mode Switching in a Compressible Rectangular Cavity Flow [J]. Aerospace, 2023, 10(6): 504. [17] KOK F N. Numerical analysis of the influence of sidewalls on full-span finite-width cavity flows [J]. ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS, 2025. [18] BERESH S J, WAGNER J L, PRUETT B O M. Particle Image Velocimetry of a Three-Dimensional Supersonic Cavity Flow[C]// 50th AIAA Aerospace Sciences Meeting.American Institute of Aeronautics and Astronautics,2012. [19] ARUNAJATESAN S, BARONE M F, WAGNER J L, et al. Joint Experimental/Computational Investigation Into the Effects of Finite Width on Transonic Cavity Flow[C]// 32nd AIAA Applied Aerodynamics Conference. Atlanta, GA:American Institute of Aeronautics and Astronautics,2014. [20] BERESH S J, WAGNER J L, PRUETT B O M, et al. Supersonic Flow over a Finite-Width Rectangular Cavity [J]. Aiaa Journal, 2014, 53(2): 296-310. [21] BERESH S J, WAGNER J L, HENFLING J F, et al. Width Effects in Transonic Flow over a Rectangular Cavity [J]. Aiaa Journal, 2015, 53(12): 1-4. [22] BERESH S J, WAGNER J L, CASPER K M. Compressibility effects in the shear layer over a rectangular cavity [J]. Journal of Fluid Mechanics, 2016, 808: 116-152. [23] CASPER K M, WAGNER J L, BERESH S J, et al. Spatial distribution of pressure resonance in compressible cavity flow [J]. Journal of Fluid Mechanics, 2018, 848: 660-675. [24] DEMAURO E P, BERESH S J, CASPER K M, et al. Volumetric Velocimetry of Complex Geometry Effects on Transonic Flow over Cavities [J]. Aiaa Journal, 2019: 1-14. [25] GEORGE B, UKEILEY L S, CATTAFESTA III L N, et al. Control of Three-Dimensional Cavity Flow Using Leading-Edge Slot Blowing[C]// 53rd AIAA Aerospace Sciences Meeting Kissimmee, Florida:American Institute of Aeronautics and Astronautics,2015. [26] ZHANG Y, ARORA N, SUN Y, et al. Suppression of Cavity Oscillations via Three-Dimensional Steady Blowing [M]. 45th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics. 2015. [27] SUN Y, TAIRA K, CATTAFESTA III L N, et al. Spanwise effects on instabilities of compressible flow over a long rectangular cavity [J]. Theoretical & Computational Fluid Dynamics, 2016. [28] SUN Y, ZHANG Y, TAIRA K, et al. Width and sidewall effects on high speed cavity flows[C]// 54th AIAA aerospace sciences meeting.American Institute of Aeronautics and Astronautics,2016: 1343. [29] SUN Y, LIU Q, CATTAFESTA III L N, et al. Effects of sidewalls and leading-edge blowing on flows over long rectangular cavities [J]. Aiaa Journal, 2019, 57(1): 106-119. [30] SINGH S, UKEILEY L S, ZHANG Y, et al. Supersonic cavity flow control using a spanwise array of leading-edge tabs [J]. Journal of Aircraft, 2022, 59(3): 788-798. [31] HANNA M, MOHANY A. Aeroacoustics and shear layer characteristics of confined cavities subject to low Mach number flow [J]. Journal of Fluids and Structures, 2023, 121: 103949. [32] BRUNNER T, KROISSENBRUNNER T, WURZINGER A, et al. Acoustic resonances and aeroacoustic feedback mechanisms occurring at a deep cavity with an overhanging lip [J]. Journal of Sound and Vibration, 2025, 606: 119004. [33] RULIK S, WRóBLEWSKI W, RUSIN K. Numerical and Experimental Analysis of the Noise Generated in a Ducted Cavity Working in Various Conditions [J]. Energies, 2021, 14. [34] RULIK S, WRóBLEWSKI W, MAJKUT M, et al. Experimental and numerical analysis of heat transfer within cavity working under highly non-stationary flow conditions [J]. Energy, 2020, 190. [35] RULIK S, WRóBLEWSKI W, NOWAK G, et al. Heat transfer intensification using acoustic waves in a cavity [J]. Energy, 2015, 87: 21-30. [36] HU Z, MAXIT L, CHENG L. Mid-to-high frequency piecewise modelling of an acoustic system with varying coupling strength [J]. Mechanical Systems and Signal Processing, 2019, 134: 106312. [37] MOHEIT L, MARBURG S. Normal Modes and Modal Reduction in Exterior Acoustics [J]. Journal of Theoretical and Computational Acoustics, 2018, 26: 1850029. [38] GINSBERG J H. Implementation of a constrained Ritz series modeling technique for acoustic cavity-structural systems [J]. The Journal of the Acoustical Society of America, 2010, 128 5: 2562-2572. [39] LAGACHE J-M, ASSAF S, SCHULTE C. Finite element synthesis of structural or acoustic receptances in view of practical design applications [J]. Journal of Sound and Vibration, 2008, 310(1): 313-351. [40] ASSAF S, LAGACHE J-M. Modal finite element synthesis of acoustic boundary receptances [J]. Mechanics & Industry, 2008, 9(6): 579-588. [41] TAM C K W. The acoustic modes of a two-dimensional rectangular cavity [J]. Journal of Sound and Vibration, 1976, 49(3): 353-364. [42] HENDERSON B S. Category 5: sound generation in viscous problems. Problem 2: sound generation by flow over a cavity[C]// Fourth Computational Aeroacoustics (CAA) Workshop on Benchmark Problems. Cleveland:NASA,2004: 71-77.

Study on flow-acoustic coupling characteristics of overhanging lip cavity considering side wall effect

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