X: Strong axis
Y: Weak axis
Z: Primary axis
Variable | Description |
---|---|
α | Rotation angle for principal axes of angle section |
A | Cross-sectional area |
Af | Area of compression flange |
As | Shear area for tubular member - pipe |
Asx | X shear area of prismatic member |
Asy | Y shear area of prismatic member |
b | Width of member (b ≤ d) |
b0 |
Distance from neutral axis to edge of web:
|
be | Effective width of structural tubing member |
bf | Width of flange |
Cb | Bending coefficient dependent upon moment gradient (section F) |
Cc | Column slenderness ratio separating elastic and inelastic buckling (section E) |
Cmx, Cmx | Coefficient applied to bending term in interaction equation (section H) |
d | Depth of member (d ≥ b) |
E | Modulus of elasticity |
E0 |
Distance of the shear center from center line of web for channel: E0 = e0 + tw / 2 |
Fa | Maximum allowable compressive stress |
Fb | Maximum allowable bending stress |
Fbx | Maximum allowable strong axis bending stress |
Fby | Maximum allowable weak axis bending stress |
Fex, Fey | Euler stress for a prismatic member divided by factor of safety |
Ft | Maximum allowable tensile stress |
Fy | Yield stress |
Fn | Maximum allowable shear stress |
fa | Computed axial stress (either tension or compression, both taken as positive) |
fb | Computed bending stress (taken as a positive quantity) |
fbx | Computed strong axis bending stress |
fby | Computed weak axis bending stress |
fvx | Computed shear stress in X direction |
fvy | Computed shear stress in Y direction |
h |
Clear distance between flanges in I-shaped members: h = d 2tf |
Ix, Iy | Moments of inertia about principal axes |
Iu, Iv | ments of inertia about principal axes of angle section member |
K | ective length factor for prismatic member |
L | Distance between cross sections braced against twist or lateral displacement of the compression flange |
Lb | Laterally unsupported length of the compression flange. |
Lc | Maximum unbraced length of the compression flange. |
Lx, Ly | L in X and Y directions |
M1, M2 | Smaller and larger moment at end of unbraced length, respectively. |
P | Axial force load |
r | Governing radius of gyration |
rT | Radius of gyration of a section comprising the compression flange plus 1/3 of the compression web area, taken about an axis in the plane of the web |
rx, ry | Radius of gyration about principal axes |
t | Thickness |
tf | Thickness of flange |
U, V | Principal axes of angle section member |
u, v | Distances from principal axes |
x, y | Offsets of centroid of angle section |
X is the strong axis, and Y is the weak axis for all I-shaped and members and channels. Tees can have either axis as their strong axis.
Category I. I-shaped members, tees and channels Section F1.1
The allowable bending stress is
Fb = 0.66 Fy | (F1-1) |
with the constraint that Lb ≤ Lc, which is given by the smaller of:
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(F1-2) |
Category II. Pipes and structural tubing Section F3.1
The allowable bending stress is
Fb = 0.66 Fy | (F3-1) |
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(F3-2) |
except, that Lc need not be less than 1200 (b/Fy), M1 is the smaller and M2 is the largest bending moments about the ends of the unbraced length, taken about the strong axis.
Category I. I-shaped members, tees and channels Section F1.2
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(F1-3) |
Category II. Pipes and structural tubing Section F3.2
Fb = 0.60 Fy | (F3-3) |
If member is in tension,
Fb = 0.60 Fy | (F1-5) |
If member is in compression, the allowable bending stress is determined as the larger value from equations (F1-6) or (F1-7) and (F1-8), with the exceptions:
When
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(F1-6) |
When
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(F1-7) |
For any value of L/rT:
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(F1-8) |
Cb is conservatively taken as unity (1.0) in equations (F1-6), (F1-7) and (F1-8).
2.A. Members with compact sections: Section F2.1
Fb = 0.75 Fy | (F2-1) |
2.B. Members with noncompact sections: Section F2.2
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(F2-3) |
Ft = 0.60 Fy | Section D1 |
Section E2
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(E2-1) |
where KL/r is the largest of KLx / rx and KLy / ry, which are equal for pipes and squares, and
![]() |
(E2-2) |
Chapter H
The following requirements must be satisfied for members experiencing both axial compression and bending:
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(H1-1) |
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(H1-2) |
When fa / Fa ≤ 0.15, Equation (H1-3) is used in lieu of Equations (H1-1) and (H1-2).
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(H1-3) |
The coefficients, also known as the Euler stress divided by safety factor, Fex and Fey are given by the following:
The coefficients Cmx and Cmy have a default value of 0.85.
The following requirements must be satisfied for members experiencing both axial tension and bending:
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(H2-1) |