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BUILDING AND STRUCTURES FORMULAS        241

                               Mn    (Cr   Mo   V)   (Ni   Cu)
                      C eq   C                                   (9.112)
                                6          5            15
             where  C   carbon content, %
                  Mn   manganese content, %
                  Cr   chromium content, %
                  Mo   molybdenum, %
                   V   vanadium, %
                  Ni   nickel content, %
                  Cu   copper, %

             To prevent underbead cracking, the weld must be cooled at an acceptable rate.
             A higher carbon equivalent requires a longer cooling rate. Refer to ASTM 6 for
             further requirements.


             STATICALLY INDETERMINATE FORCES AND MOMENTS
             IN BUILDING STRUCTURES*

             Shear, moment, and deflection formulas for statically indeterminate forces
             in rigid frames as present by Roark have the following notation: W   load,
             lb (kg); w   unit load, lb/linear in (kg/cm); M is positive when clockwise;
             V is positive when upward;  y is positive when upward. Constraining
             moments, applied couples, loads, and reactions are positive when acting as
             shown. All forces are in pounds; all moments are in inch-pounds; all deflec-
             tions and dimensions are in inches.    is in radians and tan    . I
             moment of inertia of the section of the beam with respect to the neutral axis
                        4
                             4
             of the beam, in (mm ).
               With pinned supports, concentrated load on the horizontal member, Fig. 9.9:
                        1     L 1 L 2 b   2L 2 L 3 b   3L 2 b   (b /L 3 )(L 1   L 2 )
                                                   3
                                               2
                   H      W                                      (9.113)
                                    2
                                                           3
                                          2
                                                3
                        2   L 1 L 2 L 3   L 1 L 3   L 2 L 3   L 1   (I 3 /I 1 )   L 2 (I 3 /I 2 )
                        wb   H(L 2  L 1 )
                   V 1                                           (9.114)
                             L 3
               With pinned supports, concentrated load on one vertical member, Fig. 9.10:
                      3     3     2     2
                    2L 1  2a    3ab   2L 1 L 3  2L 1 L 3 b  L 1 L 2 L 3  L 2 L 3 b

                     I 1   I 1   I 1    I 3     I 3     I 3     I 3
             H 2   W
                             3     2               3     2
                           2L 1  2L 2 L 3  2L 1 L 2 L 3  2L 1  2L 1 L 3

                            I 2   I 3      I 3    I 1    I 3
                                                                 (9.115)
                                     Wa   H 2 (L 1   L 2 )
                                 V                               (9.116)
                                           L 3
               *Roark—Formulas for Stress and Strain, McGraw-Hill.
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