Validation of an Analytical Model for the Acoustic Impedance Eduction of Multicavity Resonant Liners by a High-Fidelity Large Eddy Simulation Approach

IF 1.9 3区 工程技术 Q3 ENGINEERING, MECHANICAL
Simone Giaccherini, Lorenzo Pinelli, Michele Marconcini, Roberto Pacciani, Andrea Arnone
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Abstract

Abstract The massive growth of the air traffic during the last years is leading to stricter limitations on the noise emission levels radiated from aircraft engines. To face this issue, the installation of acoustic liners on the intake duct and the exhaust nozzles is a common strategy adopted to properly abate noise emissions coming from the fan, the compressor, the turbine, and the jet. In this context, the aim of the present article is to use high-fidelity large Eddy simulation (LES) to validate a multi-degree-of-freedom (MDOF) extension of the single-degree-of-freedom (SDOF) and double-degree-of-freedom (DDOF) analytical model provided by Hersh for impedance eduction of acoustic liners. First, the results of the original Hersh model are compared with LES calculations performed with the openfoam suite on a single-orifice and single-cavity layout (SDOF). Then the extension of the Hersh model to multicavity (MDOF) geometries by using a recursive formulation is presented. Finally, high-fidelity simulations are carried out for single-orifice and multicavity (MDOF) configurations to validate the method extension and to understand how resonant coupling and acoustic impedance are affected by multicavity resonant elements. The excellent agreement between the high-fidelity results and the analytical predictions for the single-cavity pattern confirms that the Hersh model is a useful formulation for a preliminary design of a SDOF acoustic liner. The model extension to MDOF configurations enables the designers to broaden the design space, and thus, a validated analytical method is strictly necessary to perform sensitivity studies to the multicavity geometrical parameters (i.e., facesheet thickness, cavities depth, porosity). Basically, a multicavity configuration makes the liner element resonate at different frequencies, leading to multiple absorption peaks in the audible range. In this way, the acoustic performance of the liner is extended to a wider frequency range, overcoming the limitations of a traditional SDOF configuration.
用高保真大涡模拟方法验证多腔谐振衬垫声阻抗衰减分析模型
近年来空中交通的大量增长导致对飞机发动机辐射的噪声排放水平有更严格的限制。为了解决这个问题,在进气管道和排气喷嘴上安装声学衬垫是一种常用的策略,可以适当地减少来自风扇、压缩机、涡轮和喷气机的噪音排放。在这种情况下,本文的目的是使用高保真大涡模拟(LES)来验证Hersh提供的单自由度(SDOF)和双自由度(DDOF)声学衬垫阻抗消减分析模型的多自由度(MDOF)扩展。首先,将原始Hersh模型的结果与使用单孔单腔布局(SDOF)的开放式泡沫套件进行的LES计算进行了比较。然后用递推公式将Hersh模型推广到多腔几何。最后,对单孔和多腔(MDOF)结构进行了高保真仿真,以验证方法的扩展,并了解多腔谐振单元对谐振耦合和声阻抗的影响。高保真度结果与单腔模式的分析预测之间的良好一致性证实了Hersh模型是一个有用的公式,用于SDOF声学衬垫的初步设计。将模型扩展到MDOF结构使设计人员能够扩大设计空间,因此,对多腔几何参数(即面板厚度、腔深、孔隙度)进行敏感性研究,验证的分析方法是非常必要的。基本上,多腔结构使线性元件在不同频率上共振,从而在可听范围内产生多个吸收峰。通过这种方式,衬管的声学性能扩展到更宽的频率范围,克服了传统SDOF配置的局限性。
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来源期刊
CiteScore
4.70
自引率
11.80%
发文量
168
审稿时长
9 months
期刊介绍: The Journal of Turbomachinery publishes archival-quality, peer-reviewed technical papers that advance the state-of-the-art of turbomachinery technology related to gas turbine engines. The broad scope of the subject matter includes the fluid dynamics, heat transfer, and aeromechanics technology associated with the design, analysis, modeling, testing, and performance of turbomachinery. Emphasis is placed on gas-path technologies associated with axial compressors, centrifugal compressors, and turbines. Topics: Aerodynamic design, analysis, and test of compressor and turbine blading; Compressor stall, surge, and operability issues; Heat transfer phenomena and film cooling design, analysis, and testing in turbines; Aeromechanical instabilities; Computational fluid dynamics (CFD) applied to turbomachinery, boundary layer development, measurement techniques, and cavity and leaking flows.
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