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And third, taller trees get more sun and are therefore more likely to be affected by drier edge conditions.
The present paper is concerned with the vibration of supersonic laminated plates with general edge conditions.
A shell has three fundamental identifying features, namely, the reference surface, thickness and edge conditions.
Two extreme edge conditions of simply supported and clamped edges are considered.
For free or sliding edge conditions, the fundamental mode may not be axisymmetric.
The present method is applicable to arbitrarily thick laminates and for treating arbitrary edge conditions.
The methodology is based on end effects excited when edge conditions deviate from baseline boundary data.
The critical buckling loads for elastically restrained edge conditions have been obtained.
The laminated perforated plates can be subject to free, simply supported, or clamped edge conditions.
Several combinations of simply supported, clamped and free edge conditions are considered.
For the different edge conditions, extensive spectra and directivity are presented.
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