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The limit state equations are developed from maximum stress, maximum strain, Tsai-Hill, Tsai-Wu and Hoffman failure criteria.
The maximum stress, maximum equilateral stress and deflection are the important criteria for design of the chassis.
Maximum stress, Maximum strain, Tsai-Hill and Tsai-Wu biaxial failure theories are evaluated for the assumption of isotropic behaviour and contrasted with the experimental results.
Some dimensions representing the shape of the hatch cover were selected as design variables and some design considerations related to the maximum stress, maximum deflection, and geometry of the hatch cover were selected as constraints.
The failure envelope of the experiments was compared with those of failure criteria such as those based on the maximum stress, maximum strain and ply scale continuum damage model.
The failure properties obtained experimentally from this technique are compared with the analytical predictions of the Maximum stress, Maximum strain, Tsai-Hill and Tsai-Wu failure theories and the numerical results obtained by means of the Finite Element Method.
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The maximum strain, maximum stress, Tsai Wu, Tsai Hill, Hashin and LaRC03 failure criteria are described and compared for various benchmark problems.
The new design is investigated both for maximum stress and maximum temperature.
The maximum subcutaneous stress, maximum seat-interface pressure, and maximum subcutaneous shear stress each changed with cushion thickness.
The relationship between fatigue life and maximum engineering stress, maximum strain and strain energy density were studied.
The maximum deformation and maximum stress on the silicon chip and solder bumps are evaluated.
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