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Problems in which fiber angles showed uncertainty were considered.
Layer thicknesses and fiber angles are represented by bicubic Bezier surfaces and cubic Bezier curves, respectively.
Here, we specifically investigate buckling loads for various geometric shapes and fiber angles of laminated cylinders with elliptical cross-section.
Open image in new window Fig. 10 Non-dimensional critical buckling load vs. aspect ratios and fiber angles.
Fiber angles vary spatially and result in material properties that are functions of position.
For larger fiber angles, Θ>45°, the width effects are less pronounced for both monotonic and fatigue loading.
Similar(22)
The Shepard interpolation inherently guarantees spatial continuity of fiber angle.
At lower slenderness ratios, a fiber angle of ( 0 90 ) 5 S gives higher buckling loads.
A hierarchy of parameterizations of fiber angle arrangement are constructed by using the Shepard interpolation.
A unified approach to nonlinear buckling fiber angle optimization of laminated composite shell structures is presented.
In certain cases, however, a varying fiber angle might be favorable for structural performance.
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