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                                                        CONNECTIONS


                   3.90  CHAPTER THREE

                               The design tensile rupture strength of the toe of the MC flange under the fillet is

                                                                   .
                                                              .
                                                        ×
                                                                            ×= 28 kips
                                                                        .
                                                 φR = 075 36  0 366  + 0 470    0 625 4
                                                      .
                                                            
                                                   t
                                                                 2
                               Thus the total strength of the load path in the channel flange is 834 + 28 = 862 kips > 855 kips; OK.
                                 GUSSET-TO-BRACE RUPTURE. Design strength for limit state of shear rupture of gusset is
                                                 φR v = 0.75 × 0.6 × 58 × 1.5 × 17 × 2 = 1331 kips
                               Design strength for limit state of tension rupture of gusset is
                                                     φR t = 0.75 × 58 × 1.5 × 12 = 783 kips
                               Design strength for limit state of block shear rupture of gusset is
                                          φR bs = 1331 + 0.75 × 36 × 1.5 × 12 = 1817 kips > 855 kips  OK
                                 WHITMORE SECTION. The theoretical length of the Whitmore section is (17 tan 30°)2 + 12 = 31.6 in.
                               The Whitmore section extends into the column by 5.40 in. The column web is stronger than the gus-
                               set since 1.29 × 50/36 = 1.79 > 1.5 in. The Whitmore also extends into the beam web by 6.80 in, but
                               since 0.470 × 50/36 = 0.653 < 1.5 in, the beam web is not as strong as the gusset. The effective
                               Whitmore section length is therefore taken as

                                                 l weff  = (31 .6 − . 6 80 ) + . 6 80  ×  . 0 470  ×  50  = 27 .8  in
                                                                        . 15  36
                               The effective length is based on F y = 36 ksi and the gusset thickness of 1.5 in.
                                 Since the brace force can be tension or compression, compression will control. The slenderness
                               ratio of the unsupported length of gusset is

                                                                   .
                                                          Kl  05 .  × 85 12
                                                             =          = 98 .
                                                           r      15 .
                               From the AISC Specification, Sec. J4.4, the buckling strength is
                                                          φF a = 0.9 × 36 = 32.4 ksi

                               and the buckling strength of the gusset is
                                                φR wb = 27.8 × 1.5 × 32.4 = 1350 > 855 kips  OK
                                 This completes the brace-to-gusset part of the design. Before proceeding, the distribution of
                               forces to the gusset edges must be determined. From Figs. 3.49 and 3.50,
                                               .
                                          e =  24 10  = 1205 in  e = 837 in  β  = 1225 in  α  = 150 .  in
                                                     .
                                                                             .
                                                                 .
                                          b
                                               2             c
                                                   .
                                          θ  = tan  −1 10 6875  = 41 6 .  °
                                                   12
                                                             =
                                          V =  P cos θ  = 855 0 747 638 kips
                                                       × .
                                          c
                                                          .
                                         H =  Ve  =  638 × 8 37  = 220 kips
                                               cc
                                          c
                                             e + β  12 05 +12 25
                                                           .
                                                     .
                                              b
                                         H =  P sin θ −  H = 855 0 665 220  = 349 kips
                                                                −
                                                           × .
                                                     c
                                          b
                                         M =  H e = 349  ×12 05  = 4205 in ⋅kips
                                                        .
                                                b
                                              b b
                                          b
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