Page 286 - Structural Steel Designers Handbook AISC, AASHTO, AISI, ASTM, and ASCE-07 Design Standards
P. 286

Brockenbrough_Ch06.qxd  9/29/05  5:15 PM  Page 6.8



                                                 DESIGN OF BUILDING MEMBERS


                   6.8  CHAPTER SIX

                               where (KL/r) o = column slenderness of built-up member acting as a unit
                                        α= separation ratio = h/2r ib
                                        h = distance between centroids of individual components perpendicular to member
                                           axis of buckling, in
                                        a = distance between connectors, in
                                        r ib = radius of gyration of individual angle relative to its centroidal axis parallel to
                                           member axis of buckling, in
                               In this case, h = 1.03 + 0.375 + 1.03 = 2.44 in and α= 2.44/(2 × 1.13) = 1.08. Assume maximum
                               spacing between connectors is a = 80 in. With K = 1, substitution in Eq. (6.11) yields

                                                KL   =   19 85 ×12   2   108 2   80    2
                                                         .
                                                                         .
                                                                      
                                                                             
                                                                   .
                                                r   m    166    + 082  11.  2  113   = 150
                                                                                .
                                                          .
                                                                        + 08
                               The elastic critical stress buckling stress, from Eq. (6.8), is
                                                            π 2  × 29 000
                                                                  ,
                                                      F =               = 13 90 ksi
                                                                           .
                                                       e
                                                          [( .  ×12 1 66] 2
                                                                  )/ .
                                                           19 85
                               For the determination of the critical stress F cr , since
                                             KL  =  19 85 ×12      E       29 000     
                                                                                ,
                                                  .
                                                                  .
                                                                           .
                                                                
                                             r    167   = 143 5 .    > 471  F y  = 471  36  = 133 7 .   
                                                                
                                                    .
                                                 π 2  × 29 000
                                                      ,
                                                F =       = 13 90 ksi
                                                             .
                                              e        2
                                                   143 5 .
                               The critical stress, from Eq. (6.10), is
                                                         F cr = 0.877 × 13.90 = 12.19
                               From Eqs. (6.6) and (6.7), the design strength is
                                             φP n = 0.90 × 11.7 × 12.19 = 128.4 kips > 107.5 kips  OK
                   6.8 STEEL BEAMS
                               According to the AISC Specification, the nominal capacity M p (in⋅kips) of a steel section in flexure
                               is equal to the plastic moment:
                                                                                                   (6.12)
                                                                M p = ZF y
                                                              3
                               where Z is the plastic section modulus (in ) and F y is the steel yield strength (ksi). However, this
                               applies only when local or lateral torsional buckling of the compression flange is not a governing cri-
                               terion. The nominal capacity M p is reduced when the compression flange is not braced laterally for
                               a length that exceeds the limiting unbraced length for full plastic bending capacity L p . Also, the nom-
                               inal moment capacity is less than M p when the ratio of the compression-element width to its thick-
                               ness exceeds limiting slenderness parameters for compact sections. The same is true for the effect of
                               the ratio of web depth to thickness. (See Chap. 5.)
                                 In addition to strength requirements for design of beams, serviceability is important. Deflection
                               limitations defined by local codes or standards of practice must be maintained in selecting member
                               sizes. Dynamic properties or the beams are also important design parameters in determining the
                               vibration behavior of floor systems for various uses.

                           Downloaded from Digital Engineering Library @ McGraw-Hill (www.digitalengineeringlibrary.com)
                                      Copyright © 2004 The McGraw-Hill Companies. All rights reserved.
                                       Any use is subject to the Terms of Use as given at the website.
   281   282   283   284   285   286   287   288   289   290   291