AISCAISC 360-22
Formulas

Formulas: other I-shaped members with compact or noncompact webs bent about their major axis

PDF page 447 · AISC 360-22

Formula 1

These two factors can vary from unity to as high as Mp/Myc1.6M_{p} / M_{y c} \leq 1.6 and Mp/Myt1.6M_{p} / M_{y t} \leq 1.6.

Mp/Myc1.6M_{p} / M_{y c} \leq 1.6

Formula 2

Mp/Myt1.6M_{p} / M_{y t} \leq 1.6

Formula 3

{λ=hctwSxc=Ixy;Sxt=IxdyMyc=FySxc;Myt=FySx\left\{\begin{aligned} \lambda & =\frac{h_{c}}{t_{w}} \\ S_{x c} & =\frac{I_{x}}{y} ; \quad S_{x t}=\frac{I_{x}}{d-y} \\ M_{y c} & =F_{y} S_{x c} ; \quad M_{y t}=F_{y} S_{x}\end{aligned}\right.

Formula 4

AA: Total cross-sectional area (A=Ac+At+AwA = A_c + A_t + A_w.

A=Ac+At+AwA = A_c + A_t + A_w

Formula 5

Defined by height hc=2(ytfch_c = 2(y - t_{fc}.

hc=2(ytfch_c = 2(y - t_{fc}

Formula 6

Applicable range: tfcydtftt_{fc} \leq y \leq d - t_{ft}.

tfcydtftt_{fc} \leq y \leq d - t_{ft}

Formula 7

Defined by height hp=A2Actwh_p = \frac{A - 2A_c}{t_w}.

hp=A2Actwh_p = \frac{A - 2A_c}{t_w}

Formula 8

Valid when 2AcA(Aw+2Ac2A_c \leq A \leq (A_w + 2A_c.

2AcA(Aw+2Ac2A_c \leq A \leq (A_w + 2A_c

Formula 9

λpw=hchpEFy(0.54MpMy0.09)25.70EFy\lambda_{pw} = \frac{\frac{h_c}{h_p} \sqrt{\frac{E}{F_y}}}{\left(\frac{0.54M_p}{M_y} - 0.09\right)^2} \leq 5.70 \sqrt{\frac{E}{F_y}}

Formula 10

λrw=5.70EFy\lambda_{rw} = 5.70 \sqrt{\frac{E}{F_y}}

Formula 11

If λ>λrw\lambda>\lambda_{r w}, then the web is slender and the design is governed by Section F5.

λ>λrw\lambda>\lambda_{r w}

Formula 12

The basic maximum nominal moment is RpcMyc=RpcFySxcR_{p c} M_{y c}=R_{p c} F_{y} S_{x c} corresponding to the compression flange, and RptMyt=RptFySxtR_{p t} M_{y t}=R_{p t} F_{y} S_{x t} corresponding to tension flange yielding, which is applicable only when Myt<MycM_{y t}<M_{y c} or Sxt<SxcS_{x t}<S_{x c} (beams with the larger flange in compression).

RpcMyc=RpcFySxcR_{p c} M_{y c}=R_{p c} F_{y} S_{x c}

Formula 13

RptMyt=RptFySxtR_{p t} M_{y t}=R_{p t} F_{y} S_{x t}

Formula 14

Myt<MycM_{y t}<M_{y c}

Formula 15

Sxt<SxcS_{x t}<S_{x c}

Equation C-F4-3

For a more accurate solution, especially when the loads are not applied at the centroid of the member, the designer is directed to Galambos (2001), White and Jung (2003), and Ziemian (2010). The following alternative equations in lieu of Equations F4-5 and F4-8 are provided by White and Jung:

Mn=Cbπ2EIyLb2βx2+(βx2)2+CwIy(1+0.0390JCwLb2)M_{n}=C_{b} \frac{\pi^{2} E I_{y}}{L_{b}^{2}}\left|\frac{\beta_{x}}{2}+\sqrt{\left(\frac{\beta_{x}}{2}\right)^{2}+\frac{C_{w}}{I_{y}}\left(1+0.0390 \frac{J}{C_{w}} L_{b}^{2}\right)}\right|

Equation C-F4-4

Lr=1.38EIyJSxcFL2.6βxFLSxcEJ+1+(2.6βxFLSxcEJ+1)2+27.0CwIy(FLSxcEJ)2L_{r}=\frac{1.38 E \sqrt{I_{y} J}}{S_{x c} F_{L}} \sqrt{\frac{2.6 \beta_{x} F_{L} S_{x c}}{E J}+1+\sqrt{\left(\frac{2.6 \beta_{x} F_{L} S_{x c}}{E J}+1\right)^{2}+\frac{27.0 C_{w}}{I_{y}}\left(\frac{F_{L} S_{x c}}{E J}\right)^{2}}}

where

the coefficient of monosymmetry, βx=0.9hα[(Iyc/Iyt)1]\beta_{x}=0.9 h \alpha\left[\left(I_{y c} / I_{y t}\right)-1\right], the warping constant, Cw=h2IycαC_{w}=h^{2} I_{y c} \alpha, where α=1/[(Iyc/Iyt)+1]\alpha=1 /\left[\left(I_{y c} / I_{y t}\right)+1\right], and FLF_{L} is the magnitude of the flexural stress in compression at which the lateral-torsional buckling is influenced by yielding. In Equations F4-6a and F4-6b, this stress level is taken generally as the smaller of 0.7Fy0.7 F_{y} in the compression flange, or the compression flange stress when the tension flange reaches the yield strength, but not less than 0.5Fy0.5 F_{y}.

Formula 18

where the coefficient of monosymmetry, βx=0.9hα[(Iyc/Iyt)1]\beta_{x}=0.9 h \alpha\left[\left(I_{y c} / I_{y t}\right)-1\right], the warping constant, Cw=h2IycαC_{w}=h^{2} I_{y c} \alpha, where α=1/[(Iyc/Iyt)+1]\alpha=1 /\left[\left(I_{y c} / I_{y t}\right)+1\right], and FLF_{L} is the magnitude of the flexural stress in compression at which the lateral-torsional buckling is influenced by yielding.

βx=0.9hα[(Iyc/Iyt)1]\beta_{x}=0.9 h \alpha\left[\left(I_{y c} / I_{y t}\right)-1\right]

Formula 19

Cw=h2IycαC_{w}=h^{2} I_{y c} \alpha

Formula 20

α=1/[(Iyc/Iyt)+1]\alpha=1 /\left[\left(I_{y c} / I_{y t}\right)+1\right]

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