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2.001 - MECHANICS AND MATERIALS I
                                  Lecture #6
                                  9/27/2006
                            Prof. Carol Livermore



Recall:




Sign Convention




Positive internal forces and moments shown.

Distributed Loads




                                   1
q(x) = q0

                                        L                   L
                 FTotal Loading =           q(x)dx = q0 x       = q0 L
                                    0                       0
                                        L                       L
                                                        q0 x2           q0 L2
             MADistributed Load =           q(x)xdx =               =
                                    0                     2     0         2
Lump: (Equivalent Forces)




FBD




                                             2
Fx = 0
                       R Ax = 0


                         Fy = 0
              RAy + RBy  q0 L = 0


                         MA = 0
               L
               q 0 L + RBy L = 0
               2
                         q0 L
                 R By =
                          2
Substitute:


                    q0 L
              R Ay +      q0 L = 0
                     2
                          qo L
                  R Ay =
                           2




Cut beam.




                          3
Lump:




                           Fx = 0
                       N =0


                           Fy = 0

        q0 L                           L
              q 0 x  Vy = 0  Vy q 0   x
         2                             2

                           M = 0

                q0 L          x
                    x + q0 x   +Mz = 0
                 2            2
                            L    x2
                 Mz = q0      x
                            2    2
Plot
Sanity Check
   Pinned and Pinned on rollers at end
       Cannot support moment M at ends
       Can support x and y loads  OK




                                      Fy = 0
                           Vy  (Vy + 隆Vy ) + q隆x = 0
                                   隆Vy = q隆x
                    qdVy
Limit as 隆x  0     dx



                                      M0 = 0
                                        隆x              隆x
             Mz + Mz + 隆Mz  Vy           (Vy + 隆Vy )    =0
                                         2               2
                                      隆x        隆x
                            隆Mz  2Vy     隆Vy
                                       2         2
                                               隆x
                             隆Mz = Vy 隆x  隆Vy
                                                2
                                   隆Mz     隆Vy
                              Vy =       +
                                    隆x      2
Take limit 隆x  0
                                        dMz
                                  Vy =
                                          dx
                                        dVy
                                   q=
                                         dx
But what if load is not uniformly distributed?
EXAMPLE: A more interesting structure




Q: Find all internal forces and moments in all members. Plot.

Find reactions at supports.
FBD




                                       Fx = 0
                                 RAx + RDx = 0


                                       Fy = 0
                                 RAy + RDy = 0


                                      MA = 0
                              M  RDx L + RDy L = 0
FBD
This is a 2-force member.
                                            L
                             R Ay               1
                                  = tan 慮 = 2 =
                             R Ax           L   2
                                            R Ax
                            RAx = 2RAy          =2
                                            R Ay
                                  R Ax
                                       = 1
                                  R Dx
                                  R Ay
                                       = 1
                                  R Dy
                                 R Ax   R Ay
                                      =
                                 R Dx   R Dy
                                 R Ax   R Dx
                                      =
                                 R Ay   R Dy
So:
                            R Ax
                                 = 2  RDx = 2RDy
                            R Dy
So:
                                         M
                                  R Dy =
                                          L
                                          M
                                 R Ay = 
                                           L
                                         2M
                                 R Dx =
                                          L
                                        2M
                                 R Ax =
                                          L

                                       Fx = 0
                                R Ax  R C x = 0
                                          2M
                                 RCx =
                                           L

                                       Fy = 0
                                R Ay  R C y = 0
                                          M
                                 R Cy =
                                           L




                                   7
Take cut

FBD




                      Fx = 0
                    2M
               N       =0
                     L
                      2M
                   N=
                       L

                      Fy = 0
                   M
                      Vy = 0
                   L
                        M
                   Vy =
                         L

                     M = 0
               M
                 x + Mz = 0
               L
                     M
               Mz =      x
                      L
FBD of Cut 2




                       8
Fx = 0
                      M
                       +N =0
                      L
                         M
                      N=
                          L

                       Fy = 0
                  2M
                       Vy = 0
                   L
                         2M
                   Vy =
                          L

                       M = 0
                   M    2M
               Mz +  x    x=0
                   L     L
                           2x
               Mz = M 1 
                           L
FBD of Cut 3




                       Fx = 0
                      M
                       +N =0
                      L
                         M
                      N=
                          L

                       Fy = 0
                  2M
                      Vy = 0
                   L




                         9
2M
                     Vy =
                             L

                         M = 0
                     2M
                 Mz +   x=0
                      L
                       2M
                  Mz =    x
                        L
FBD of Cut 4




                         Fx = 0
                     M
                      +N =0
                     L
                        M
                     N=
                         L

                         Fy = 0
                  2M
                       Vy = 0
                   L
                         2M
                   Vy =
                          L

                         M = 0
                   2M
               M     x + Mz = 0
                    L
                            2x
               Mz = M 1 
                            L




                    10
Lec6   MECH ENG  STRucture

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  • 1. 2.001 - MECHANICS AND MATERIALS I Lecture #6 9/27/2006 Prof. Carol Livermore Recall: Sign Convention Positive internal forces and moments shown. Distributed Loads 1
  • 2. q(x) = q0 L L FTotal Loading = q(x)dx = q0 x = q0 L 0 0 L L q0 x2 q0 L2 MADistributed Load = q(x)xdx = = 0 2 0 2 Lump: (Equivalent Forces) FBD 2
  • 3. Fx = 0 R Ax = 0 Fy = 0 RAy + RBy q0 L = 0 MA = 0 L q 0 L + RBy L = 0 2 q0 L R By = 2 Substitute: q0 L R Ay + q0 L = 0 2 qo L R Ay = 2 Cut beam. 3
  • 4. Lump: Fx = 0 N =0 Fy = 0 q0 L L q 0 x Vy = 0 Vy q 0 x 2 2 M = 0 q0 L x x + q0 x +Mz = 0 2 2 L x2 Mz = q0 x 2 2 Plot
  • 5. Sanity Check Pinned and Pinned on rollers at end Cannot support moment M at ends Can support x and y loads OK Fy = 0 Vy (Vy + 隆Vy ) + q隆x = 0 隆Vy = q隆x qdVy Limit as 隆x 0 dx M0 = 0 隆x 隆x Mz + Mz + 隆Mz Vy (Vy + 隆Vy ) =0 2 2 隆x 隆x 隆Mz 2Vy 隆Vy 2 2 隆x 隆Mz = Vy 隆x 隆Vy 2 隆Mz 隆Vy Vy = + 隆x 2 Take limit 隆x 0 dMz Vy = dx dVy q= dx But what if load is not uniformly distributed?
  • 6. EXAMPLE: A more interesting structure Q: Find all internal forces and moments in all members. Plot. Find reactions at supports. FBD Fx = 0 RAx + RDx = 0 Fy = 0 RAy + RDy = 0 MA = 0 M RDx L + RDy L = 0 FBD
  • 7. This is a 2-force member. L R Ay 1 = tan 慮 = 2 = R Ax L 2 R Ax RAx = 2RAy =2 R Ay R Ax = 1 R Dx R Ay = 1 R Dy R Ax R Ay = R Dx R Dy R Ax R Dx = R Ay R Dy So: R Ax = 2 RDx = 2RDy R Dy So: M R Dy = L M R Ay = L 2M R Dx = L 2M R Ax = L Fx = 0 R Ax R C x = 0 2M RCx = L Fy = 0 R Ay R C y = 0 M R Cy = L 7
  • 8. Take cut FBD Fx = 0 2M N =0 L 2M N= L Fy = 0 M Vy = 0 L M Vy = L M = 0 M x + Mz = 0 L M Mz = x L FBD of Cut 2 8
  • 9. Fx = 0 M +N =0 L M N= L Fy = 0 2M Vy = 0 L 2M Vy = L M = 0 M 2M Mz + x x=0 L L 2x Mz = M 1 L FBD of Cut 3 Fx = 0 M +N =0 L M N= L Fy = 0 2M Vy = 0 L 9
  • 10. 2M Vy = L M = 0 2M Mz + x=0 L 2M Mz = x L FBD of Cut 4 Fx = 0 M +N =0 L M N= L Fy = 0 2M Vy = 0 L 2M Vy = L M = 0 2M M x + Mz = 0 L 2x Mz = M 1 L 10