A hybrid numerical approach to predict the vibrational responses of panels excited by a turbulent boundary layer

M. Karimi, P. Croaker, L. Maxit, O. Robin, A. Skvortsov, S. Marburg, N. Kessissoglou

Research output: Contribution to journalArticlepeer-review

35 Scopus citations

Abstract

In this work, a hybrid numerical approach to predict the vibrational responses of planar structures excited by a turbulent boundary layer is presented. The approach combines an uncorrelated wall plane wave technique with the finite element method. The wall pressure field induced by a turbulent boundary layer is obtained as a set of uncorrelated wall pressure plane waves. The amplitude of these plane waves are determined from the cross spectrum density function of the wall pressure field given either by empirical models from literature or from experimental data. The response of the planar structure subject to a turbulent boundary layer excitation is then obtained from an ensemble average of the different realizations. The numerical technique is computationally efficient as it rapidly converges using a small number of realizations. To demonstrate the method, the vibrational responses of two panels with simply supported or clamped boundary conditions and excited by a turbulent flow are considered. In the case study comprising a plate with simply supported boundary conditions, an analytical solution is employed for verification of the method. For both cases studies, numerical results from the hybrid approach are compared with experimental data measured in two different anechoic wind tunnels.

Original languageEnglish
Article number102814
JournalJournal of Fluids and Structures
Volume92
DOIs
StatePublished - Jan 2020

Keywords

  • Finite element method
  • Flow-induced vibration
  • Turbulent boundary layer
  • Uncorrelated wall plane wave

Fingerprint

Dive into the research topics of 'A hybrid numerical approach to predict the vibrational responses of panels excited by a turbulent boundary layer'. Together they form a unique fingerprint.

Cite this