Strength Theories

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Strength Theories The majority of material strength data is based on uniaxial tensile test results. Usually, all that you have to work with is the yield strength Sy and/or the ultimate tensile strength Su. This is fine if you only have the one normal stress component present : this is true for simple tension or compression members and for parts loaded only in bending. σ σ 1 = σx 1 In this case, failure (defined as the onset of plastic deformation) occurs when σx = σ1 =Sy/n ‘n’ is the factor of safety. In many loading cases, we have more than just one normal stress component. E.g. in torsion, we have a single shear stress component: τ τ xy xy Or, combined bending and torsion in a shaft: τ xy σ x σx τxy These cases can all be reduced to a simple biaxial case by finding the principal stresses, σ and σ 1 2 σ 2 σ σ1 1 σ 2 Now when does failure occur? For ductile materials there are two commonly used strength theories - the Maximum Shear Stress (MSS) or Tresca theory and the von Mises or Distortion Energy theory. Strength Theories 1. Maximum Shear Stress: This states that failure occurs when the maximum shear stress in the component being designed equals the maximum shear stress in a uniaxial tensile test at the yield stress: This gives τmax = Sy/2n or | σ1 – σ2 | = Sy/n or | σ2 – σ3 | = Sy/n or | σ3 – σ1 | = Sy/n whichever of the last three leads to the safest result. The latter usually involves σ3 being zero, i.e. plane stress, and both σ1 and σ2 having the same sign. Note that the yield strength is reduced by the factor of safety ‘n’. 2. von Mises or Distortion Energy Theory: This states that failure occurs when the von Mises stress σe in the component being designed equals the von Mises stress σe in a uniaxial tensile test at the yield stress: 2 2 2 0.5 This gives: σe = √2/2 [( σ1 – σ2 ) + ( σ2 – σ3 ) + ( σ3 – σ1 ) ] = Sy/n In the plane stress case we have σ3 = 0 and hence: 2 2 0.5 σe = [σ1 – σ1σ2 + σ2 ] = Sy/n This is the most commonly used of the strength equations. A third theory, the Maximum Normal Stress theory is similarly defined. It must NEVER be used for design with ductile materials. A modified version of this theory is sometimes used with brittle materials. All three of these theories are shown on a plot the σ1 versus σ2 below: Strength Theories .

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