{"title":"Acoustic energy balances for sound radiated from duct exit with mean flow","authors":"S. Rienstra","doi":"10.1177/1475472X221107363","DOIUrl":null,"url":null,"abstract":"An old model problem for the exchange of energy between sound field and mean flow by vortex shedding has been worked out in numerical detail. The analytically exact solution of the problem of reflection, diffraction and radiation of acoustic modes in a semi-infinite annular duct with uniform subsonic mean flow, including shedding of unsteady vorticity from the duct exit, allows a precise formulation of Myers’ energy for perturbations of an inviscid mean flow. The transmitted power P t in the duct and the radiated power P f in the far field differ by the amounts of hydrodynamic far field powers P H i inside and P H o outside the wake (vortex sheet) emanating from the duct edge, plus the power P w that disappears into the vortex sheet. This last component represents the source term in Myers’ energy equation. This is evidence of the non-conserved character of acoustic energy in mean flow, owing to the coupling of the acoustic field with the mean flow. P f , P H i and P H o are always positive. This is normally the case too for P w and P t . But for not too high frequencies or other circumstances where shed vorticity produces more sound than was necessary for its creation, P w and even P t may also be negative.","PeriodicalId":49304,"journal":{"name":"International Journal of Aeroacoustics","volume":"21 1","pages":"410 - 429"},"PeriodicalIF":1.2000,"publicationDate":"2022-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Aeroacoustics","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.1177/1475472X221107363","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"ACOUSTICS","Score":null,"Total":0}
引用次数: 1
Abstract
An old model problem for the exchange of energy between sound field and mean flow by vortex shedding has been worked out in numerical detail. The analytically exact solution of the problem of reflection, diffraction and radiation of acoustic modes in a semi-infinite annular duct with uniform subsonic mean flow, including shedding of unsteady vorticity from the duct exit, allows a precise formulation of Myers’ energy for perturbations of an inviscid mean flow. The transmitted power P t in the duct and the radiated power P f in the far field differ by the amounts of hydrodynamic far field powers P H i inside and P H o outside the wake (vortex sheet) emanating from the duct edge, plus the power P w that disappears into the vortex sheet. This last component represents the source term in Myers’ energy equation. This is evidence of the non-conserved character of acoustic energy in mean flow, owing to the coupling of the acoustic field with the mean flow. P f , P H i and P H o are always positive. This is normally the case too for P w and P t . But for not too high frequencies or other circumstances where shed vorticity produces more sound than was necessary for its creation, P w and even P t may also be negative.
本文对涡旋脱落声场与平均流能量交换的一个老模型问题进行了数值计算。具有均匀亚音速平均流的半无限环形管道中声模的反射、衍射和辐射问题的解析精确解,包括管道出口的非定常涡量的脱落,允许对无粘平均流的扰动的迈尔斯能量的精确公式。管道内的传输功率pt和远场辐射功率pf的差异在于,从管道边缘发出的尾迹(旋涡片)内部和外部的流体动力远场功率ph i的量加上消失在旋涡片中的功率pw。最后一个分量表示Myers能量方程中的源项。由于声场与平均流的耦合作用,声能在平均流中具有非守恒性。P f, P H i和P H o总是正的。对于pw和pt通常也是这样。但如果频率不太高,或者在其他情况下,流涡产生的声音比产生它所必需的声音要多,那么pw甚至pt也可能是负的。
期刊介绍:
International Journal of Aeroacoustics is a peer-reviewed journal publishing developments in all areas of fundamental and applied aeroacoustics. Fundamental topics include advances in understanding aeroacoustics phenomena; applied topics include all aspects of civil and military aircraft, automobile and high speed train aeroacoustics, and the impact of acoustics on structures. As well as original contributions, state of the art reviews and surveys will be published.
Subtopics include, among others, jet mixing noise; screech tones; broadband shock associated noise and methods for suppression; the near-ground acoustic environment of Short Take-Off and Vertical Landing (STOVL) aircraft; weapons bay aeroacoustics, cavity acoustics, closed-loop feedback control of aeroacoustic phenomena; computational aeroacoustics including high fidelity numerical simulations, and analytical acoustics.