Abstract
The geometric nonlinear response of a tapered, clamped ceramic matrix composite (CMC) panel to narrowband Gaussian random excitations was investigated. The effects of the coupling between the bending and axial strain response, resulting from the through-the-thickness asymmetry of the panel taper were observed. The axial strain power spectral density (PSD) exhibited sharp peaks at the primarily bending natural frequencies of the panel.
Original language | English (US) |
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Pages (from-to) | 1682-1687 |
Number of pages | 6 |
Journal | AIAA journal |
Volume | 40 |
Issue number | 8 |
DOIs | |
State | Published - Aug 2002 |
ASJC Scopus subject areas
- Aerospace Engineering