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Maximum Moment of a Non-Compact Or Slender
Webbed I
Beam Or Channel: |
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Calculation: |
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Designer/Checker: |
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Input: |
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(Note: All input Metric units are converted to English units
for the equations below and then the output English units are converted back to
Metric) |
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From AISC F4 And F5: |
This calculation applies to: (a) doubly symmetric I-shaped members bent about
their major axis with noncompact webs; and (b) singly symmetric I-shaped members
with webs attached to the mid-width of the flanges, bent about their major axis,
with compact or noncompact webs; and (c) doubly symmetric and singly symmetric
I-shaped members with slender webs attached to the mid-width of the flanges,
bent about their major axis. |
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Unbraced length (Lb - ft or m) |
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Limiting laterally unbraced length for the limit state of yielding (Lp - ft or m) |
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Steel yield strength (fy - ksi or MPa) |
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Limiting laterally unbraced length for the limit state of inelastic
lateral-torsional buckling (Lr - ft or m) |
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Depth of the beam (d - in or mm) |
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Depth of the area in compression (y - in or mm) |
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Thickness of the compression flange (tfc - in or mm) |
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Width of the compression flange (bfc - in or mm) |
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Effective radius of gyration (rt - in or mm)* |
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Lateral-torsional buckling modification factor (Cb)** |
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Moment of inertia, x-axis (Ix - in^3 or mm^3) |
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Height of web (h - in or mm) |
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Thickness of web (tw - in or mm) |
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Width to thickness ratio of the flange (WTF = bf/2tf) |
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Limiting slenderness of compact flange (WTFp) |
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Limiting slenderness of noncompact flange (WTFr) |
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*Effective radius of gyration, rts, can be conservatively approximated
for I shapes with a rectangular compression flange
as the radius of gyration of a section of the compression flange plus 1/3 of
the compression web area. |
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**Cb can be conservatively taken as 1.00. |
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Output: |
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Maximum moment of the beam, Mu = |
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