Page 83 - Marks Calculation for Machine Design
P. 83

P1: Sanjay
                          January 4, 2005
                                      16:18
        Brown.cls
                 Brown˙C02
                              U.S. Customary     BEAMS            SI/Metric        65
                    Step 3. Calculate the maximum bending  Step 3. Calculate the maximum bending
                    moment (M max ) from Eq. (2.27) as  moment (M max ) from Eq. (2.27) as
                             wL 2  (750 1b/ft)(6ft) 2          wL 2  (10,000 N/m)(1.8m) 2
                       M max =  √  =    √               M max =  √  =      √
                             9  3      9  3                   9  3        9  3
                             27,000 ft · lb                   32,400 N · m
                           =          = 1,732 ft · lb       =          = 2,078 N · m
                               15.59                             15.59
                    Step 4. Figure 2.42 shows that this maximum  Step 4. Figure 2.42 shows that this maximum
                    bending moment (M max ) of 1,732 ft · lb is  bending moment (M max ) of 2,078 N · mis
                    located at                         located at
                             L                                 L
                         x = √  = 0.577 L                 x = √  = 0.577 L
                              3                                 3
                                            L                                  L
                          = 0.577 (6ft) = 3.46 ft >         = 0.577 (1.8m) = 1.04 m >
                                            2                                  2
                    from the left end of the beam.     from the left end of the beam.
                                                                          w

                             A                                           B
                                               ∆

                                                   L
                             FIGURE 2.43  Beam deflection diagram.

                    Deflection. For this loading configuration, the deflection ( ) along the beam is shown in
                    Fig. 2.43, and given by Eq. (2.28) for values of the distance (x) from the left end of the
                    beam,
                                             wx    4     2 2    4
                                         =       (7L − 10L x + 3x )             (2.28)
                                           360 EIL
                    where   = deflection of beam (positive downward)
                         w = applied triangular load
                         x = distance from left end of beam
                         L = length of beam
                         E = modulus of elasticity of beam material
                         I = area moment of inertia of cross-sectional area about axis through centroid

                      The maximum deflection (  max ) caused by this loading configuration is given by
                    Eq. (2.29),

                                         wL 4
                               max = 0.00652    at  x =  1 −  8  15  L ≈ (0.52) L  (2.29)
                                          EI
                    located at the point (approximately 0.52 L) from the left end of the beam.
   78   79   80   81   82   83   84   85   86   87   88