{"title":"Scaling laws for the sound generation of bio-inspired flapping wings","authors":"Li Wang, Xueyue Ji, John Young, Fang-Bao Tian","doi":"arxiv-2409.00900","DOIUrl":null,"url":null,"abstract":"Bio-inspired flapping wings have been extensively studied for their\nremarkable aerodynamic performance. Recently, their noise emission has\nattracted growing interest, but a careful analysis of scaling laws for their\nsound generation is missing. This work presents scaling laws for the sound\ngeneration of bio-inspired flapping wings during hovering flight based on the\npotential flow theory and Ffowcs Williams-Hawkings acoustic analogy. Direct\nnumerical simulations considering a range of parameters including the Reynolds\nnumber, Mach number and wing kinematics confirms that the proposed scaling laws\ncapture the major physics involved and their predictions agree well with the\nnumerical results. The scaling laws can be used as a powerful tool for\nengineers in the design of micro-aerial vehicles considering both aerodynamics\nand acoustics performances simultaneously.","PeriodicalId":501125,"journal":{"name":"arXiv - PHYS - Fluid Dynamics","volume":"15 1","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2024-09-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"arXiv - PHYS - Fluid Dynamics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/arxiv-2409.00900","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
Bio-inspired flapping wings have been extensively studied for their
remarkable aerodynamic performance. Recently, their noise emission has
attracted growing interest, but a careful analysis of scaling laws for their
sound generation is missing. This work presents scaling laws for the sound
generation of bio-inspired flapping wings during hovering flight based on the
potential flow theory and Ffowcs Williams-Hawkings acoustic analogy. Direct
numerical simulations considering a range of parameters including the Reynolds
number, Mach number and wing kinematics confirms that the proposed scaling laws
capture the major physics involved and their predictions agree well with the
numerical results. The scaling laws can be used as a powerful tool for
engineers in the design of micro-aerial vehicles considering both aerodynamics
and acoustics performances simultaneously.