Page 90 - Handbook of Civil Engineering Calculations, Second Edition
P. 90

STATICS, STRESS AND STRAIN, AND FLEXURAL ANALYSIS  1.73

                              5. Place the system in the position thus established,
                              and compute V de
                              Thus, R L   50(100   6   13.8)/200   23.1 kips (102.75 kN). The load at panel point d is
                              P d   5(6)/25 1.2 kips (5.34 kN); V de   23.1   1.2   21.9 kips (97.41 kN).
                              6. Assume left-to-right locomotion; proceed as in step 3
                              Consider that load 4 is within panel de and the remaining loads are to the right of this pan-
                              el. Proceeding as in step 3, we find dV de /dx   15(7/200)   35(   1/200) > 0.
                                So, as the system moves from left to right, V de is maximum at the instant that load 4 is at e.
                              7. Place the system in the position thus established, and
                              compute V de
                              Thus V de   R L   [50(100   8.2)1/200   23.0 kips (102.30 kN);   V de, max   23.0 kips
                              (102.30 kN).
                              8. Compute the maximum tensile force in De
                              Using the same relation as in step 3 of the previous calculation procedure, we find csc
                                           2 0.5
                                        2
                                   2
                                [(25   30 )/30 ]    1.30; then De   23.0(1.30)   29.9-kip (133.00-kN) tension.
                              INFLUENCE LINE FOR BENDING MOMENT
                              IN BRIDGE TRUSS

                              The Warren truss in Fig. 50a supports a bridge at its top chord. Draw the influence line
                              for the bending moment at b caused by a moving load traversing the bridge floor.

































                                FIGURE 50
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