Page 265 - Marks Calculation for Machine Design
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                                      14:56
                          January 4, 2005
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                 Brown˙C06
                                     STATIC DESIGN AND COLUMN BUCKLING
                      Forbrittlematerials,therearethreestaticdesigntheoriesthatfittheavailableexperimental
                    data on whether the combinations of (σ 1 ,σ 2 ) for a machine element are safe:  247
                      Maximum-normal-stress theory
                      Coulomb-Mohr theory
                      Modified Coulomb-Mohr theory
                      Each of these three theories will be discussed separately, followed by the appropriate
                    recommendations as to which theory is best for every possible combination of the principal
                    stresses (σ 1 ,σ 2 ). Remember, combinations in the second (II) quadrant are impossible if it is
                    assumed that the maximum principal stress (σ 1 ) is always greater than or at least equal to
                    the minimum principal stress (σ 2 ), even though the mathematical expressions and graphical
                    representations that will be shown allow this combination.
                    Maximum-Normal-Stress Theory. The square in Fig. 6.10 represented by the respective
                    values of the tensile and compressive strengths shown in Fig. 6.1 is the graphical representa-
                    tion of the maximum-normal-stress theory of static failure. Any combination of the principal
                    stresses (σ 1 ) and (σ 2 ) that are inside the square is a safe design and any combination outside
                    the square is unsafe. Remember, the strengths (S ut )and (S uc ) are positive values.


                                                   s 2





                                                   S ut

                                                  II   I
                                                                       s 1
                                 –S uc                      S ut
                                                  III  IV








                                                  –S uc


                          FIGURE 6.10  Maximum-normal-stress theory (brittle).

                      The mathematical expressions representing a safe design according to the maximum-
                    normal-stress theory are given in Eq. (6.13),

                                          σ 1 < S ut  or σ 2 > − S uc           (6.13)
                    where the first expression in Eq. (6.13) results in a boundary at the vertical line, (σ 1 = S ut ),
                    and the second expression results in a boundary at the horizontal line at, (σ 2 =−S uc ).
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