Which theory of failure will you use for aluminum components under steady loading?
AMaximum principal stress theory
BMaximum shear stress theory
CMaximum strain energy theory
DMaximum principal strain theory
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Related Questions:
A cold-rolled steel shaft is designed on the basis of the maximum shear stress theory. The Principal stresses induced at its critical section are 50 MPa and -50 MPa respectively. If the yield stress for the shaft material is 400 MPa, the factor of safety of the design is
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Consider the following statements :Which of the statements is/are correct?
- Based on the experiment results, the distortion energy theory predicts the failure of a component made of ductile material most accurately.
- According to the distortion energy theory, the shear yield strength is less than the shear strength in tension.
At a point in a structure, there are two mutually perpendicular tensile stresses of 800 N/cm² and 400 N/cm². If the Poisson's ratio is 0.25, what would be the equivalent stress in simple tension according to maximum principal strain theory?
Which theory of failure represents the given statement?
'The failure will occur in a material when the maximum principal strain reaches the strain due to yield stress in simple tension or when the minimum principal strain reaches the strain due to yield stress in simple compression.'