Page 86 - Handbook of Civil Engineering Calculations, Second Edition
P. 86

STATICS, STRESS AND STRAIN, AND FLEXURAL ANALYSIS  1.69

                              Calculation Procedure:

                              1. Determine the magnitude of the resultant and its location
                              Since the member carries only concentrated loads, the maximum moment at any instant
                              occurs under one of these loads. Thus, the problem is to determine the position of the load
                              system that causes the absolute maximum moment.
                                The magnitude of the resultant R is R   10   4   15   29 kips (129.0 kN). To deter-
                              mine the location of R, take moments with respect to A (Fig. 47). Thus  M A   29AD
                              4(5)   15(17), or AD   9.48 ft (2.890 m).
                              2. Assume several trial load positions
                              Assume that the maximum moment occurs under the 10-kip (44.5-kN) load. Place the
                              system in the position shown in Fig. 47b, with the 10-kip (44.5-kN) load as far from the
                              adjacent support as the resultant is from the other support. Repeat this procedure for the
                              two remaining loads.
                              3. Determine the support reactions for the trial load positions
                              For these three trial positions, calculate the reaction at the support adjacent to the load un-
                              der consideration. Determine whether the vertical shear is zero or changes sign at this
                              load. Thus, for position 1: R L   29(15.26)/40   11.06 kips (49.194 kN). Since the shear
                              does not change sign at the 10-kip (44.5-kN) load, this position lacks significance.
                                Position 2: R L   29(17.76)/40   12.88 kips (57.290 kN). The shear changes sign at the
                              4-kip (17.8-kN) load.
                                Position 3: R R   29(16.24)/40   11.77 kips (52.352 kN). The shear changes sign at
                              the 15-kip (66.7-kN) load.
                              4. Compute the maximum bending moment associated with
                              positions having a change in the shear sign
                              This applies to positions 2 and 3. The absolute maximum moment is the larger of these
                              values. Thus, for position 2: M   12.88(17.76)   10(5)   178.7 ft·kips (242.32 kN·m).
                              Position 3: M   11.77(16.24)   191.1 ft·kips (259.13 kN·m). Thus, M max   191.1 ft·kips
                              (259.13 kN·m).
                              5. Determine the absolute maximum shear
                              For absolute maximum shear, place the 15-kip (66.7-kN) load an infinitesimal distance
                              to the left of the right-hand support. Then V max   29(40   7.52)/40   23.5 kips (104.53 kN).
                                When the load spacing is large in relation to the beam span, the absolute maximum
                              moment may occur when only part of the load system is on the span. This possibility re-
                              quires careful investigation.



                              INFLUENCE LINE FOR SHEAR IN A
                              BRIDGE TRUSS

                              The Pratt truss in Fig. 48a supports a bridge at its bottom chord. Draw the influence line
                              for shear in panel cd caused by a moving load traversing the bridge floor.

                              Calculation Procedure:
                              1. Compute the shear in the panel being considered with a unit
                              load to the right of the panel
                              Cut the truss at section YY. The algebraic sum of vertical forces acting on the truss at pan-
                              el points to the left of YY is termed the shear in panel cd.
   81   82   83   84   85   86   87   88   89   90   91