| Summary: | 碩士 === 國立台灣工業技術學院 === 機械工程技術研究所 === 85 === This paper studied the oscillations of a plate subjected to both
the aerodynamic pressure and the in-plane force . The
aerodynamic pressure may be considered as a white noise or non-
white noise Gaussian process and the in-plane force is simulated
to be a small randomness white noise Gaussian process . In the
analysis , the variances of displacement responses of the plate
are evaluated by the recursive method . The effects of small
randomness on the in-plane forces are investigated by using the
perturbation technique . The response statistics of plate are
also determined as functions of length-to-width ratio , mean of
in-plane forces , aerodynamic pressure parameter , and air-to-
structure mass ratio . The numerical results are compared with
those given in the reference papers.
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