Structural response of stiffened plates in similitude under a turbulent boundary layer excitation

被引:19
|
作者
Franco, Francesco [1 ]
Berry, Alain [2 ]
Petrone, Giuseppe [1 ]
De Rosa, Sergio [1 ]
Ciappi, Elena [3 ]
Robin, Olivier [2 ]
机构
[1] Univ Napoli Federico II, Pasta Lab, Dept Ind Engn, Via Claudio 21, I-80125 Naples, Italy
[2] Univ Sherbrooke, Grp Acoust, Dept Genie Mecan, Univ Sherbrooke GAUS, Sherbrooke, PQ J1K 2R1, Canada
[3] CNR INM Inst Marine Engn, Via Vallerano 139, I-00128 Rome, Italy
关键词
Similitude laws; Stiffened plates; Stochastic structural response; Turbulent boundary layer load; WALL-PRESSURE FLUCTUATIONS; VIBRATION RESPONSE; FLAT; LAWS;
D O I
10.1016/j.jfluidstructs.2020.103119
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In structural dynamics, similitude laws usually deal with simple configurations as thin flat plates with point forces. Only recently, few papers have analyzed stiffened shells or stochastic pressure loads. This research activity extends the applicability of some similitude laws, developed for thin flat plates under a turbulent boundary layer load, to ribbed plates forced by the same wall pressure fluctuations. The work addresses the problem of designing a scaled experimental test-article and, successively, of re-modulating the measured data in order to get the structural response of an original (unscaled) configuration. Due to the complexity of the structural domain, the design of a scaled configuration leads to a distorted similitude. Then, a simple approach, to circumvent the distortion effects, is proposed. (c) 2020 Elsevier Ltd. All rights reserved.
引用
收藏
页数:13
相关论文
共 50 条
  • [1] Similitude laws for the structural response of flat plates under a turbulent boundary layer excitation
    Franco, Francesco
    Robin, Olivier
    Ciappi, Elena
    De Rosa, Sergio
    Berry, Alain
    Petrone, Giuseppe
    MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2019, 129 : 590 - 613
  • [2] Similitude laws for the vibroacoustic response of fluid-loaded plates under a turbulent boundary layer excitation
    Plouseau-Guede, Xavier
    Berry, Alain
    Maxit, Laurent
    Meyer, Valentin
    JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 2025, 157 (01): : 595 - 605
  • [3] VIBROACOUSTIC PERFORMANCE OF A STIFFENED PLATE WITH PERFORATION UNDER THE EXCITATION OF TURBULENT BOUNDARY LAYER
    Li Piao
    Li Yukun
    Zhang Jingyu
    Chen Meixia
    Wang Ting
    PROCEEDINGS OF ASME 2024 43RD INTERNATIONAL CONFERENCE ON OCEAN, OFFSHORE AND ARCTIC ENGINEERING, OMAE2024, VOL 5B, 2024,
  • [4] RADIATION EFFICIENCY OF DAMPED PLATES UNDER TURBULENT BOUNDARY LAYER EXCITATION
    Kou, Yiwei
    Liu, Bilong
    Tian, Jing
    PROCEEDINGS OF THE 22ND INTERNATIONAL CONGRESS ON SOUND AND VIBRATION: MAJOR CHALLENGES IN ACOUSTICS, NOISE AND VIBRATION RESEARCH, 2015, 2015,
  • [5] The random structural response due to a turbulent boundary layer excitation
    De Rosa, S
    Franco, F
    Romano, G
    Scaramuzzino, F
    WIND AND STRUCTURES, 2003, 6 (06) : 437 - 450
  • [6] Vibroacoustic behavior of submerged stiffened composite plates excited by a turbulent boundary layer
    Zhou, Zhenlong
    Mei, Zhiyuan
    Wu, Dajiang
    Chen, Guotao
    JOURNAL OF SOUND AND VIBRATION, 2022, 528
  • [7] Vibroacoustic behavior of submerged stiffened composite plates excited by a turbulent boundary layer
    Zhou, Zhenlong
    Mei, Zhiyuan
    Wu, Dajiang
    Chen, Guotao
    Journal of Sound and Vibration, 2022, 528
  • [8] The effect of concentrated masses on the response of a plate under a turbulent boundary layer excitation
    De Rosa, S.
    Franco, F.
    Capasso, D.
    Costagliola, S.
    MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2011, 25 (04) : 1192 - 1203
  • [9] STRUCTURAL EXCITATION BY A TURBULENT BOUNDARY-LAYER - AN OVERVIEW
    LEEHEY, P
    JOURNAL OF VIBRATION ACOUSTICS STRESS AND RELIABILITY IN DESIGN-TRANSACTIONS OF THE ASME, 1988, 110 (02): : 220 - 225
  • [10] STRUCTURAL EXCITATION BY A TURBULENT BOUNDARY LAYER: AN OVERVIEW.
    Leehey, P.
    Journal of vibration, acoustics, stress, and reliability in design, 1988, 110 (02): : 220 - 225