Experimental and Numerical Investigation of Novel Acoustic Liners and Their Design for Aero-Engine Applications

被引:0
|
作者
Neubauer, Moritz [1 ]
Genssler, Julia [2 ]
Radmann, Vincent [3 ]
Kohlenberg, Fleming [2 ]
Pohl, Michael [4 ]
Boehme, Kurt [1 ]
Knobloch, Karsten [5 ]
Sarradj, Ennes [3 ]
Hoeschler, Klaus [4 ]
Modler, Niels [1 ]
Enghardt, Lars [2 ]
机构
[1] Tech Univ Dresden, Inst Lightweight Engn & Polymer Technol ILK, Holbeinstr 3, D-01307 Dresden, Germany
[2] Tech Univ Berlin, Inst Fluid Dynam & Engn Acoust, Muller Breslau Str 8, D-10623 Berlin, Germany
[3] Tech Univ Berlin, Inst Fluid Dynam & Engn Acoust, Einsteinufer 25, D-10587 Berlin, Germany
[4] Brandenburg Univ Technol Cottbus Senftenberg, Chair Aero Engine Design, Siemens Halske Ring 14, D-03046 Cottbus, Germany
[5] German Aerosp Ctr DLR, Inst Prop Technol, Engine Acoust, Muller Breslau Str 8, D-10623 Berlin, Germany
关键词
acoustic liner; plate resonator; Helmholtz resonator; broadband noise; honeycomb structure; model; curved design; HELMHOLTZ RESONATOR; NOISE-CONTROL; MECHANICAL-PROPERTIES; PLATE SILENCER; STRENGTH; OPTIMIZATION; REFLECTION; BEHAVIOR;
D O I
10.3390/aerospace10010005
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents a combined experimental and numerical investigation on a novel liner concept for enhanced low-frequency and broadband acoustic attenuation. In particular, two different realizations, derived from conventional Helmholtz resonators (HR) and plate resonators (PR) are investigated, which both deploy flexible materials with material inherent damping. In this context, a comprehensive experimental investigation was carried out focusing the identification and evaluation of various geometric parameters and material properties on the acoustics dissipation and related properties of various materials in a simplified setup of a single Helmholtz resonator with flexible walls (FHR concept). Furthermore, a parameter study based on analytical models was performed for both liner concepts, taking into account material as well as geometric parameters and their effects on transmission loss. In addition, design concepts that enable cylindrical or otherwise curved liner structures and the corresponding manufacturing technologies are presented, while considering essential structural features such as drainage. With respect to the potential application in jet engines, a structural-mechanical analysis considering the relevant load cases to compare and discuss the mechanical performance of a classical HR and the FHR concept liner is presented. Finally, both concepts are evaluated and possible challenges and potentials for further implementation are described.
引用
收藏
页数:24
相关论文
共 50 条
  • [21] Numerical Simulation of Aero-Engine Lubrication System
    Lu, Yaguo
    Liu, Zhenxia
    Huang, Shengqin
    Xu, Tao
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2009, 131 (03):
  • [22] Investigation of entropy noise in aero-engine combustors
    Bake, Friedrich
    Michel, Ulf
    Roehle, Ingo
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2007, 129 (02): : 370 - 376
  • [23] NUMERICAL INVESTIGATION OF TRANSIENT SOOT EVOLUTION PROCESSES IN AN AERO-ENGINE MODEL COMBUSTOR
    Eberle, Christian
    Gerlinger, Peter
    Geigle, Klaus Peter
    Aigner, Manfred
    COMBUSTION SCIENCE AND TECHNOLOGY, 2015, 187 (12) : 1841 - 1866
  • [24] Investigation of entropy noise in aero-engine combustors
    Bake, Friedrich
    Michel, Ulf
    Roehle, Ingo
    Proceedings of the ASME Turbo Expo 2006, Vol 1, 2006, : 67 - 76
  • [25] Numerical analysis of the dynamic flame response of a spray flame for aero-engine applications
    Innocenti, Alessandro
    Andreini, Antonio
    Facchini, Bruno
    Peschiulli, Antonio
    INTERNATIONAL JOURNAL OF SPRAY AND COMBUSTION DYNAMICS, 2017, 9 (04) : 310 - 329
  • [26] Optimal microphone selection for aero-engine acoustic measurement
    Li, Zepeng
    Qiao, Baijie
    Wen, Bi
    Chen, Xuefeng
    Jakobsson, Andreas
    AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 148
  • [27] Back-to-back comparison of impedance measurement techniques applied to the characterization of aero-engine nacelle acoustic liners
    Ferrante, Piergiorgio
    De Roeck, Wim
    Desmet, Wim
    Magnino, Nicola
    APPLIED ACOUSTICS, 2016, 105 : 129 - 142
  • [28] Experimental validation of the beat vibration of aero-engine
    Ding X.
    Liao M.
    Peng D.
    Han F.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2023, 38 (11): : 2639 - 2647
  • [29] Experimental and numerical analysis on vibration features of typical external pipe in aero-engine
    Cheng G.
    Wang X.
    Wang G.
    International Journal of Wireless and Mobile Computing, 2019, 17 (01): : 101 - 114
  • [30] Intermetallic Materials for Automotive and Aero-engine Applications
    Clemens, H.
    BHM Berg- und Huttenmannische Monatshefte, 2008, 153 (09): : 337 - 341