Sentence examples for greater buckling load from inspiring English sources

By investigating the corresponding lengths versus aspect ratios, which result in greater buckling load with angle-ply laminates than cross-ply, curve-fitting gives a relation y = 5 x 2 - 21 x + 42.

In addition, the slenderness ratio for each aspect ratio was calculated for the cases of having a greater buckling load with angle-ply n S than symmetric-cross-ply ( 0 / 90 / ⋯ ) n S, and this was also expressed as numerical equations.  .

Antisymmetric quasi-isotropic laminates, based on 0, 90 and ±45° angles produces greater buckling loads than the equivalent symmetric lay-up.

For symmetric angle-ply, the greatest buckling load occurred at the reinforcement angle of ±60 75°.

Figure 12 compares different modes of buckling deformations for various aspect ratios with a fiber angle of ( 75 - 75 ) 5 S, which showed the greatest buckling load documented in Table 4.

Results reveal that the fiber-reinforced composite cylindrical skirt laminated symmetrically with both cross-ply layers [0/90°] and angle-ply layers [+45/−45°] can sustain a great buckling load.

The influence of stitches is evaluated by examining buckling and failure for panels with failure loads up to 3.5 times greater than buckling loads.

The skin thickness has great impact on the buckling load and the final failure load.

The experimental results show that the equivalent compression stiffness of I-shape stiffener has great influence on the buckling load and failure mode of stiffened panel, but a little effect on the failure load of stiffened panel.

With more stacks of struts and connectivity at nodes, the restriction must be stronger and the buckling load is greater.

By comparing and analyzing this phenomenon for various aspect ratios and slenderness ratios, an equation was suggested, which expresses the base line where buckling load becomes greater at angle-ply than cross-ply.