AISCAISC 360-22
Formulas

Formulas: Slender Element Members Excluding Round HSS

PDF page 434 · AISC 360-22

Equation C-E7-1

be=1.92tEf(10.34(b/t)Ef)bb_{e}=1.92 t \sqrt{\frac{E}{f}\left(1-\frac{0.34}{(b / t)} \sqrt{\frac{E}{f}}\right)} \leq b

where

  • E=modulusE=\operatorname{modulus} of elasticity, ksi (MPa)
  • b=b= width of stiffened compression element, in. (mm)
  • ff = critical stress when slender element is not considered, ksi (MPa)
  • t=t= thickness of element, in. (mm)

Equation C-E7-2

This may be compared with the generalized effective width, Equation E7-3:

be=b(1c1FelFn)FelFnb_{e}=b\left(1-c_{1} \sqrt{\frac{F_{e l}}{F_{n}}}\right) \sqrt{\frac{F_{e l}}{F_{n}}}

where

FelF_{e l} is the local elastic buckling stress, and c1c_{1} is the empirical correction factor typically associated with imperfection sensitivity. The two expressions are essentially equivalent if one recognizes that

Equation C-E7-3

Fel=kπ2E12(1v2)(tb)2F_{e l}=k \frac{\pi^{2} E}{12\left(1-\mathrm{v}^{2}\right)}\left(\frac{t}{b}\right)^{2}

where

v=Poisson s\mathrm{v}=\mathrm{Poisson}^{\prime} \mathrm{~s} ratio

= 0.3

Formula 4

and utilizes k=4.0k=4.0 for the stiffened element, c1=0.18c_{1}=0.18 for the imperfection sensitivity factor, and sets f=Fnf=F_{n}.

f=Fnf=F_{n}

Formula 5

At the limiting width-to-thickness ratio, λ=λr,b=be\lambda=\lambda_{r}, b=b_{e}, and Fel=FelrF_{e l}=F_{e l-r}; therefore, at this limit, local elastic buckling implies

λ=λr,b=be\lambda=\lambda_{r}, b=b_{e}

Formula 6

Fel=FelrF_{e l}=F_{e l-r}

Equation C-E7-4

Felr=kπ2E12(1v2)(tb)2=kπ2E12(1v2)(1λr)2F_{e l-r}=k \frac{\pi^{2} E}{12\left(1-\mathrm{v}^{2}\right)}\left(\frac{t}{b}\right)^{2}=k \frac{\pi^{2} E}{12\left(1-\mathrm{v}^{2}\right)}\left(\frac{1}{\lambda_{r}}\right)^{2}

Equation C-E7-6

which may be used to back-calculate the plate buckling coefficient, kk, assumed in Table B4.1a:

k=(114c12c1)212(1v2)π2FyEλr2k=\left(\frac{1-\sqrt{1-4 c_{1}}}{2 c_{1}}\right)^{2} \frac{12\left(1-\mathrm{v}^{2}\right)}{\pi^{2}} \frac{F_{y}}{E} \lambda_{r}^{2}

Equation C-E7-7

This relationship provides a prediction of the elastic local buckling stress consistent with the kk implicit in Table B4.1a, after substitution:

Fel=(114c12c1λrλ)2Fy=(c2λrλ)2FyF_{e l}=\left(\frac{1-\sqrt{1-4 c_{1}}}{2 c_{1}} \frac{\lambda_{r}}{\lambda}\right)^{2} F_{y}=\left(c_{2} \frac{\lambda_{r}}{\lambda}\right)^{2} F_{y}

Equation C-E7-8

be=(1c1c2λrλFyFn)c2λrλFyFnbb_{e}=\left(1-c_{1} c_{2} \frac{\lambda_{r}}{\lambda} \sqrt{\frac{F_{y}}{F_{n}}}\right) c_{2} \frac{\lambda_{r}}{\lambda} \sqrt{\frac{F_{y}}{F_{n}}} b

Equation C-E7-9

be=(10.24λrλFyFn)1.31λrλFyFnbb_{e}=\left(1-0.24 \frac{\lambda_{r}}{\lambda} \sqrt{\frac{F_{y}}{F_{n}}}\right) 1.31 \frac{\lambda_{r}}{\lambda} \sqrt{\frac{F_{y}}{F_{n}}} b

Equation C-E7-10

be=(10.28λrλ1FyF)1.38λrλ1FyFbb_{e}=\left(1-0.28 \frac{\lambda_{r}}{\lambda_{1}} \sqrt{\frac{F_{y}}{F}}\right) 1.38 \frac{\lambda_{r}}{\lambda_{1}} \sqrt{\frac{F_{y}}{F}} b

Equation C-E7-11

be=(10.33λrλFyFn)1.49λrλFyFnbb_{e}=\left(1-0.33 \frac{\lambda_{r}}{\lambda} \sqrt{\frac{F_{y}}{F_{n}}}\right) 1.49 \frac{\lambda_{r}}{\lambda} \sqrt{\frac{F_{y}}{F_{n}}} b

Equation C-E7-12

be=c2c3tkcEFn(1c1c2c3(b/t)kcEFn)b_{e}=c_{2} c_{3} t \sqrt{\frac{k_{c} E}{F_{n}}}\left(1-\frac{c_{1} c_{2} c_{3}}{(b / t)} \sqrt{\frac{k_{c} E}{F_{n}}}\right)

where

c3c_{3} is the constant associated with slenderness limits given in Table B4.1a (Geschwindner and Troemner, 2016). Combining the constants in Equation C-E7-12 with c4=c2c3c_{4}=c_{2} c_{3} and c5=c1c2c3c_{5}=c_{1} c_{2} c_{3} yields

Formula 15

Combining the constants in Equation C-E7-12 with c4=c2c3c_{4}=c_{2} c_{3} and c5=c1c2c3c_{5}=c_{1} c_{2} c_{3} yields

c4=c2c3c_{4}=c_{2} c_{3}

Formula 16

c5=c1c2c3c_{5}=c_{1} c_{2} c_{3}

Equation C-E7-13

be=c4tkcEFn(1c5(b/t)kcEFn)b_{e}=c_{4} t \sqrt{\frac{k_{c} E}{F_{n}}}\left(1-\frac{c_{5}}{(b / t)} \sqrt{\frac{k_{c} E}{F_{n}}}\right)

Found in

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