Nonlinear panel response by a monte carlo approach

Published

Journal Article

The vibration of clamped and simply supported elastic panels due to subsonic and supersonic turbulent boundarylayer flows is investigated by a Monte Carlo technique. The resulting generalized random forces are simulated numerically from boundary-layer turbulence spectra and the response analysis is performed in time domain. The mutual interaction between panel motion and external and/or internal airflow is included. Response studies are performed with respect to rms response, probability structure, peak distribution, threshold crossing and spectral density. The effect on the response statistics of in-plane loading, static pressure differential and cavity pressure is investigated. © 1974 American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

Full Text

Duke Authors

Cited Authors

  • Vaicaitis, R; Dowell, EH; Ventres, CS

Published Date

  • January 1, 1974

Published In

Volume / Issue

  • 12 / 5

Start / End Page

  • 685 - 691

International Standard Serial Number (ISSN)

  • 0001-1452

Digital Object Identifier (DOI)

  • 10.2514/3.49320

Citation Source

  • Scopus