Page 269 - Marks Calculation for Machine Design
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P1: Shibu
                          January 4, 2005
                                      14:56
                 Brown˙C06
        Brown.cls
                                     STATIC DESIGN AND COLUMN BUCKLING
                    Remember that for brittle materials, the ultimate strength in compression is significantly
                    greater than the ultimate strength in tension.                251
                    Recommendations for Brittle Materials.  Based on the closeness of the fit of the experi-
                    mental data shown in Fig. 6.13, the following are the recommendations as to which theory
                    best predicts whether a design is safe or not, specifically in the first (I) and fourth (IV)
                    quadrants.
                      First (I): (σ 1 > 0 and σ 2 > 0)
                      Maximum-normal-stress theory is the most accurate. Coulomb-Mohr theory does not
                      apply. Modified Coulomb-Mohr theory does not apply.
                      Fourth (IV): (σ 1 > 0 and 0 >σ 2 > −S ut )
                      Maximum-normal-stress theory is the most accurate. Coulomb-Mohr theory is okay,
                      but conservative. Modified Coulomb-Mohr theory does not apply.
                      Fourth (IV):  (σ 1 > 0 and −S ut >σ 2 > −S uc )
                      Modified Coulomb-Mohr theory is the most accurate. Coulomb-Mohr theory is okay, but
                      conservative. Maximum-normal-stress theory does not apply.
                    Graphically, these recommendations are shown in Fig. 6.14.
                               ◦
                      The line at 45 passing through the origin of the coordinate system in Fig. 6.14 establishes
                    the left boundary of the possible combinations of the principal stresses (σ 1 , σ 2 ). The vertical
                    line in the first (I) quadrant that extends downward to (−S ut ) in the fourth (IV) quadrant, and




                                                   s 2
                                  Boundary of allowable
                                     combinations
                                                         Maximum-normal-stress
                                                               theory
                                                   S ut

                                                   II    I  S
                                                             ut
                                                                       s 1
                                 –S uc
                                                       IV
                                                 –S ut
                                                                 Coulomb-Mohr
                                                                    theory
                                               III

                                                           Modified Coulomb-Mohr
                                                  –S uc          theory
                              Maximum-normal-stress
                                    theory


                          FIGURE 6.14  Summary of recommendations (brittle).
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