YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Turbulence Noise of Slat Trailing Edge Controlled by Porous Material

    Source: Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 004::page 04025051-1
    Author:
    Peixun Yu
    ,
    Wei Zhang
    ,
    Jie Zhou
    ,
    Xiao Han
    ,
    Yuefei Li
    ,
    Yandong Wu
    DOI: 10.1061/JAEEEZ.ASENG-5997
    Publisher: American Society of Civil Engineers
    Abstract: The utilization of porous materials is regarded as an effective strategy for mitigating aerodynamic noise at the trailing edge. In this study, a two-step computational fluid mechanics/computational aeroacoustics (CFD/CAA) hybrid method was employed to evaluate the noise impact of porous materials located at the trailing edge of high-lift slats. The turbulence field variable information was extracted from steady-state volume-averaged Navier-Stokes (VANS) equations using a spatial filter model based on Euler discretization, which generated turbulence velocity and determined the broadband noise source term. The linear Euler equation (LEE) with a source term was utilized to compute sound wave propagation in the fluid region, while the volume-averaged linearized Euler equation (VALEE) was applied for sound wave propagation in the porous region. Prior to conducting calculations and analyses, we validated our self-developed solver’s flow field computations in porous media against commercial software Fluent. Subsequently, verification of our method’s accuracy involved comparing synthetic turbulence velocities generated by the spatial filter model with two-point intercorrelation data from two-dimensional uniform and inhomogeneous artificial turbulence. Finally, we confirmed the applicability of Darcy terms and Forchheimer terms for sound propagation in homogeneous and anisotropic porous media as part of our study. Based on the establishment of an effective numerical model, the flow field and sound field of porous materials embedded at various positions within the slats were calculated and analyzed. The noise reduction effects of porous materials located in different areas exhibited significant variations. When the trailing edge of the slat was fully embedded with porous material, the turbulent kinetic energy at that location increased due to interactions between the porous material and the incoming shear layer airflow, leading to an increase in noise levels. Conversely, when only a portion of the tail edge of the slat was embedded with porous material, there was a notable reduction in slat noise; specifically, the sound pressure level (SPL) decreased by approximately 5 dB across most directions.
    • Download: (7.870Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Turbulence Noise of Slat Trailing Edge Controlled by Porous Material

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4307065
    Collections
    • Journal of Aerospace Engineering

    Show full item record

    contributor authorPeixun Yu
    contributor authorWei Zhang
    contributor authorJie Zhou
    contributor authorXiao Han
    contributor authorYuefei Li
    contributor authorYandong Wu
    date accessioned2025-08-17T22:31:50Z
    date available2025-08-17T22:31:50Z
    date copyright7/1/2025 12:00:00 AM
    date issued2025
    identifier otherJAEEEZ.ASENG-5997.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4307065
    description abstractThe utilization of porous materials is regarded as an effective strategy for mitigating aerodynamic noise at the trailing edge. In this study, a two-step computational fluid mechanics/computational aeroacoustics (CFD/CAA) hybrid method was employed to evaluate the noise impact of porous materials located at the trailing edge of high-lift slats. The turbulence field variable information was extracted from steady-state volume-averaged Navier-Stokes (VANS) equations using a spatial filter model based on Euler discretization, which generated turbulence velocity and determined the broadband noise source term. The linear Euler equation (LEE) with a source term was utilized to compute sound wave propagation in the fluid region, while the volume-averaged linearized Euler equation (VALEE) was applied for sound wave propagation in the porous region. Prior to conducting calculations and analyses, we validated our self-developed solver’s flow field computations in porous media against commercial software Fluent. Subsequently, verification of our method’s accuracy involved comparing synthetic turbulence velocities generated by the spatial filter model with two-point intercorrelation data from two-dimensional uniform and inhomogeneous artificial turbulence. Finally, we confirmed the applicability of Darcy terms and Forchheimer terms for sound propagation in homogeneous and anisotropic porous media as part of our study. Based on the establishment of an effective numerical model, the flow field and sound field of porous materials embedded at various positions within the slats were calculated and analyzed. The noise reduction effects of porous materials located in different areas exhibited significant variations. When the trailing edge of the slat was fully embedded with porous material, the turbulent kinetic energy at that location increased due to interactions between the porous material and the incoming shear layer airflow, leading to an increase in noise levels. Conversely, when only a portion of the tail edge of the slat was embedded with porous material, there was a notable reduction in slat noise; specifically, the sound pressure level (SPL) decreased by approximately 5 dB across most directions.
    publisherAmerican Society of Civil Engineers
    titleTurbulence Noise of Slat Trailing Edge Controlled by Porous Material
    typeJournal Article
    journal volume38
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-5997
    journal fristpage04025051-1
    journal lastpage04025051-17
    page17
    treeJournal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 004
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian