Nonlinear response and fatigue of stiffened panels

Siu-Tong Choi, Rimas Vaicaitis

研究成果: Article同行評審

7 引文 斯高帕斯(Scopus)


The surface protection systems of aerospace and aircraft structures are often constructed from discretely stiffened panels. The information that is available indicates that response of surface panels exposed to high intensity surface flow and/or acoustic pressure is nonlinear. A theoretical study on nonlinear response of discretely stiffened panels to random pressures and thermal loads is presented in this paper. The random pressures are simulated in time-space domain and the nonlinear equations of motion are solved numerically by a Monte Carlo type approach. In addition, preliminary estimates of sonic fatigue based on the nonlinear stress distribution of response peaks and fatigue data from constant amplitude tests are given. The numerical results include deflection and stress response time histories, spectral densities, root mean square values, crossing rates, probability distribution, peak distribution and fatigue damage.

頁(從 - 到)150-160
期刊Probabilistic Engineering Mechanics
出版狀態Published - 1989 1月 1

All Science Journal Classification (ASJC) codes

  • 統計與非線性物理學
  • 土木與結構工程
  • 核能與工程
  • 凝聚態物理學
  • 航空工程
  • 海洋工程
  • 機械工業


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