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Compendium of Design Office Problems said:"4.2 Lateral Bracing of Continuous Beam When does a point of inflection constitute a safe lateral bracing point for computation of the allowable bending stress in the bottom flange of a continuous beam?"
Compendium of Design Office Problems said:Lateral Bracing of Continuous Beams
Does a point of inflection constitute a safe "lateral bracing point" for computation of the allowable bending stress in the bottom flange of a continuous beam? Are there any other guidelines for this issue?
1999 AISC Specification said:For beams with double curvature, the inflection point can not be considered a brace point because twist occurs at that point (Galambos, 1998).
Compendium of Design Office Problems said:Lateral Bracing of Continuous Beams
Does a point of inflection constitute a safe ‘‘lateral bracing point’’ for computation of the lateral-torsional buckling flexural strength of a continuous beam? Are there any other guidelines for this issue?
Response
A flexural point of inflection occurs in a beam where there is a change in curvature from negative to positive. Even though at this point the value of the moment is zero, it is not equivalent to a brace point.
The American Institute of Steel Construction (AISC) (1994) notes this distinction in the commentary (Section F1, "Design for Flexure," pp. 195–199) where it states that "the length between braces, not the distance to inflection points, and C[sub]b[/sub] is used in the resistance equation." Also, Ricles and Walsh (1993) note the necessity for providing bracing at the point of inflection.
Section B.6 of the AISC specification requires "at points of support, beams, girders and trusses shall be restrained against rotation about their longitudinal axis (AISC 1994). In addition, lateral or rotational restraint must be provided along the beam length if the beam is assumed to be fully braced. For continuous beams, restraint is necessary for that portion of the bottom flange, which is in compression. Restraint may be provided by the joists themselves depending on the relative proportions of the assembly. A procedure for calculating the restraint is described by Essa and Kennedy (1995) and Rongoe (1996).