Page 57 - Marks Calculation for Machine Design
P. 57

P1: Sanjay
                          January 4, 2005
                                      16:18
        Brown.cls
                 Brown˙C02
                              U.S. Customary     BEAMS            SI/Metric        39
                    solution                           solution
                    Step 1. Calculate the maximum shear force  Step 1. Calculate the maximum shear force
                    (V max ) from Eq. (2.1) as         (V max ) from Eq. (2.1) as
                             F   12,000 lb                     F   55,000 N
                       V max =  =      = 6,000 lb         V max =  =      = 27,500 N
                             2     2                           2      2
                    Step 2. As shown in Fig. 2.13, this maximum  Step 2. As shown in Fig. 2.13, this maximum
                    shear force (V max ) of 6,000 lb does not have a  shear force (V max ) of 27,500 N does not have a
                    specific location.                  specific location.
                    Step 3. Calculate the maximum bending  Step 3. Calculate the maximum bending
                    moment (M max ) from Eq. (2.3) as  moment (M max ) from Eq. (2.3) as
                             FL  (12,000 lb)(6ft)              FL  (55,000 N)(2m)
                      M max =  =                         M max =  =
                             4        4                        4        4
                             72,000 ft · lb                    110,000 N · m
                           =         = 18,000 ft · lb        =           = 27,500 N · m
                                4                                  4
                    Step 4. Figure 2.14 shows that this maximum  Step 4. As shown in Fig. 2.14, this maximum
                    bending moment (M max ) of 18,000 ft · lb is  bending moment (M max ) of 27,500 N · mis
                    located at the midpoint of the beam.  located at the midpoint of the beam.
                                         L/2         F

                              A                ∆                          B

                                                    L
                              FIGURE 2.15  Beam deflection diagram.

                    Deflection. For this loading configuration, the deflection ( ) along the beam is shown in
                    Fig. 2.15, and given by Eq. (2.4) for values of distance (x) from the left end of the beam,
                                          Fx    2    2            L
                                       =      (3L − 4x )  0 ≤ x ≤                (2.4)
                                         48 EI                    2
                    where   = deflection of beam
                         F = applied force at midpoint of beam
                         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
                      Note that the distance (x) in Eq. (2.4) must be between 0 and half the length of the
                    beam (L/2). As the deflection is symmetrical about the midpoint of the beam, values of the
                    distance (x) greater than the length (L/2) have no meaning in this equation.
                      The maximum deflection (  max ) caused by this loading configuration is given by
                    Eq. (2.5),
                                                FL 3          L
                                           max =       at  x =                   (2.5)
                                                48 EI         2
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