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LRFD-Steel Design

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LRFD-Steel Design Dr. Ali I. Tayeh First Semester Steel Design Dr. Ali I. Tayeh Chapter 6-B Beam-Columns Beam-Columns Beam-Columns Beam-Columns Beam-Columns Beam ... – PowerPoint PPT presentation

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Title: LRFD-Steel Design


1
LRFD-Steel Design
  • Dr.
  • Ali I. Tayeh
  • First Semester

2
Steel DesignDr. Ali I. Tayeh
  • Chapter 6-B

3
Beam-Columns
Example 6.5
Solution
4
Beam-Columns
5
Beam-Columns
6
Beam-Columns
7
Beam-Columns
8
Beam-Columns
Example 6.6
9
Beam-Columns
Solution
10
Beam-Columns
11
Beam-Columns
12
Beam-Columns
13
Beam-Columns
14
Beam-Columns
  • MEMBERS IN UNBRACED FRAMES
  • In a beam column whose ends are free to
    translate, the maximum primary moment resulting
    from the side sway is almost always at one end.
    As was illustrated in the next Figure the maximum
    secondary moment from the sides way is always at
    the end. As a consequence of this condition, the
    maximum primary and secondary moments are usually
    additive and there is no need for the factor Cm
    in effect, Cm 1.0.
  • The amplification factor for the sides way
    moments, B2, is given by two equations.
  • Either may be used the choice is usually one of
    convenience
  • OR

15
Beam-Columns
  • Evaluation of Cm
  • The summations for Pu and Pe2apply to all columns
    that are in the same story as the column under
    consideration. The rationale for using the
    summations is that B2

16
Beam-Columns
Design of beam column The procedure can be
plained as following
17
Beam-Columns
Evaluation of Cm
18
Beam-Columns
  • The detailed procedure for design is
  • Select an average b value from Table 6-1 (if
    bending appears more dominant than axial load,
    select a value of m instead). If weak axis
    bending is present, also choose a value of n.
  • From Equation 6.5 or 6.6, solve for m or h.
  • Select a shape from Table 6-2 that has values of
    b, nt, and n close to those needed. These values
    are based on the assumption that weak axis
    buckling control the axial compressive strength
    and that Ch1.0.
  • See Example 6.8

19
Beam-Columns
  • See Example 6.8
  • Solution

20
Beam-Columns
21
Beam-Columns
22
Beam-Columns
23
Beam-Columns
  • Design of Bracing
  • A frame can be braced to resist directly applied
    lateral forces or to provide stability. The
    latter type, stability bracing, The stiffness
    and strength requirements for stability can be
    added directly to the requirements for directly
    applied loads .
  • Frame bracing can be classified as nodal or
    relative. With nodal bracing, lateral support is
    provided at discrete locations and does not
    depend on the support from other part of the
    frame.
  • The AISC requirements for stability bracing are
    given in Section C3 of the Specification. For
    frames, the required strength is

24
Beam-Columns
See Example 6.11
25
Beam-Columns
  • Design of Unbraced Beam-Columns
  • The preliminary design of beam-columns in braced
    frames has been illustrated. The amplification
    factor BI was assumed to be equal to 1.0 for
    purposes of selecting a trial shape B I could
    then be evaluated for this trial shape. In
    practice, BI with almost always be equal to 1.0.
    For beam-columns subject to sides way, the
    amplification factor B2 is based on several
    quantities that may not be known until all column
    in the frame have been selected. If AISC Equation
    C 1-4 is used for B2, the sides way deflection
    ?oh may not be available for a preliminary
    design. If AISC Equation Cl-5 is used, ? Pe2may
    not be known. The following methods are suggested
    for evaluating H2.

26
Beam-Columns
  • Design of Un braced Beam-Columns
  • in the United States contains a limit on the
    drift index, values of 1/500 to 1/200arc commonly
    used (Ad Hoc Committee on Serviceability, 1986).
    Remember that ?oh is the drift caused by IH, so
    if the drift index is based on service loads,
    then the lateral loads H must also be service
    loads. Use of a prescribed drift index enables
    the designer to determine the final value of B2
    at the outset.
  • See Example 6.12

27
Beam-Columns
  • TRUSSES WITH TOP-CHORD LOADS BETWEEN JOINTS
  • If a compression member in a truss must support
    transverse loads between its ends, it will be
    subjected to bending as well as axial compression
    and is therefore a beam-column. This condition
    can occur in the top chord of a roof truss with
    purlins located between the joints. The top chord
    of an open-web steel joist must also be designed
    as a beam-column because an open-web steel joist
    must support uniformly distributed gravity loads
    on its top chord. To account for loadings of this
    nature, a truss can be modeled as an assembly of
    continuous chord members and pin-connected web
    members. The axial loads and bending moments can
    then be found by using a method of structural
    analysis such as the stiffness method. The
    magnitude of the moments involved, however, does
    not usually warrant this degree of
    sophistication, and in most cases an approximate
    analysis will suffice.

28
Beam-Columns
  • TRUSSES WITH TOP-CHORD LOADS BETWEEN JOINTS
  • The following procedure is recommended.
  • Consider each member of the top chord to be a
    fixed-end beam. Use the fixed end moment as the
    maximum bending moment in the member. The top
    chord is actually one continuous member rather
    than a series of individual pin-connected
    members, so this approximation is more accurate
    than treating each member as a simple beam.
  • Add the reactions from this fixed-end beam to the
    actual joint loads to obtain total joint loads.
  • Analyze the truss with these total joint loads
    acting. The resulting axial load in the top-chord
    member is the axial compressive load to be used
    in the design.

29
Beam-Columns
  • TRUSSES WITH TOP-CHORD LOADS BETWEEN JOINTS
  • This method is represented schematically in the
    next figure . Alternatively, the bending moments
    and beam reactions can be found by treating the
    top chord as a continuous beam with supports at
    the panel points.
  • See Example 6.13

30
Beam-Columns -Steel Design
  • End
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