Sentence examples for maximum buckling loads from inspiring English sources

The critical buckling load of the shell is obtained by summation of the maximum buckling loads of supporting nodes.

Results show that the minimum buckling load obtained corresponds to the largest ratio a/b = 1 (circular notch), while maximum buckling loads correspond to the smallest ratio of the geometric defect a/b.

Optimum laminate configuration for the maximum buckling load of filament-wound laminated conical shells is investigated.

A generalized reciprocal approximation is presented for design of variable-stiffness laminated composite panels for maximum buckling load.

Subsequently, the cylinder is optimized to carry a maximum buckling load under bending, while applying a strength constraint.

Permutation genetic algorithms optimizing the stacking sequence of a composite laminate for maximum buckling load are studied.

A variable stiffness composite cylinder made by fiber steering is optimized for maximum buckling load due to pure bending.

Here, strength constraints are considered in maximum buckling load design, to ensure that the failure load is greater than the buckling load.

A procedure to design symmetrically laminated structures for maximum buckling load with manufacturing uncertainty in the ply angle which is the design variable, is described.

It is shown that three layers in the shell are sufficient to achieve the maximum buckling load in most practically important cases.

Subsequently, preliminary optimisation of VAT plates for maximum buckling load is done using the proposed definition of non-linear variation of fibre angles.