Page 255 - Marks Calculation for Machine Design
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P1: Shibu
                                      14:56
                          January 4, 2005
        Brown.cls
                 Brown˙C06
                                                                                  237
                                     STATIC DESIGN AND COLUMN BUCKLING
                    minimum principal stress (σ 2 ). Also, combinations in the third (III) quadrant require that
                    the minimum principal stress (σ 2 ) be at least equal to or more negative than the maximum
                    principal stress (σ 1 ).
                      The factor-of-safety (n) for this theory is given in Eq. (6.6), which replaces the inequality
                    sign in Eq. (6.5) with an equal to sign, then rearranged to give
                                               σ 1 − σ 2  1
                                                      =                          (6.6)
                                                 S y    n
                      An alternate expression commonly used in place of Eq. (6.6) for the factor-of-safety (n)
                    for the maximum-shear-stress theory can be defined using the maximum shear stress (τ max )
                    and the yield strength in shear (S sy ) from Eq. (6.4) as
                                                 τ max  1
                                                     =                           (6.7)
                                                 S sy  n
                    Distortion-Energy Theory.  Without presenting the many steps in its development that
                    can be found in any number of references, the expression given in Eq. (6.8) represents the
                    combinations of the principal stresses (σ 1 , σ 2 ) for a safe design according to the distortion-
                    energy theory.
                                             2
                                                 2
                                            σ + σ − σ 1 σ 2 < S 2 y              (6.8)
                                                 2
                                             1
                      The expression in Eq. (6.8) represents the equation of an ellipse inclined at 45 as shown
                                                                             ◦
                    in Fig. 6.4. Surprisingly, this ellipse passes through the six corners of the enclosed shape
                                                            Maximum-normal-stress
                                                   s 2
                                                                  theory
                                                   S y
                                 Maximum-shear-stress
                                       theory

                                                           I
                                                  II
                                        –S y
                                                                       s 1
                                                                 S y
                                                       IV
                                               III               Distortion-energy
                                                                     theory
                                                          Maximum-shear-stress
                                                   –S y         theory
                             Maximum-normal-stress
                                   theory


                          FIGURE 6.4  Distortion-energy theory (ductile).
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