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BEAMS
A structural member loaded in the transverse direction to the longitudinal axis.
Internal Forces:Bending Moments and Shear
Limit States
Load Deflection
0
50
100
150
200
250
300
350
400
450
500
0 4 8 12 16 20 24
Deflection (in)
Lo
ad
(k
ips
)
FEM Test
Classification of Shapes
Compact Section
Non-Compact Section
Web Local Buckling
Flange Local Buckling
Bending Strength of Compact Shapes
Elastic Buckling
pxcrn MSFM
27.0
76.6117.0
95.1
EJc
hSF
hS
Jc
F
ErLL oxy
oxytsrb
2
2
2
078.01
ts
b
oxtsb
bcr r
L
hS
Jc
rL
ECF
xyr SFM 7.0
Elastic Buckling
Cb = factor to account for non-uniform bending within the unbraced length
L/4 L/4 L/4 L/4
A B C
Mmax
0.33435.2
5.12
max
max
mCBA
b RMMMM
MC
See AISC table 3-1 p 3.10
Elastic Buckling
Cb = factor to account for non-uniform bending within the unbraced length
0.33435.2
5.12
max
max
mCBA
b RMMMM
MC
Rm= 1 for doubly symmetric cross sections and singly symmetric subject to single curvature
See textbook p 190 for other cases
Elastic Buckling
Cb = factor to account for non-uniform bending within the unbraced length
2
2
2
078.01
ts
b
oxtsb
bcr r
L
hS
Jc
rL
ECF
Elastic Buckling
Cb = factor to account for non-uniform bending within the unbraced length
x
wyts S
CIr 2
channelsfor
2
shapes I symmetricdoubly for 1
w
yo
C
Ihc
ho = distance between flange centroids = d-tf
Bending Strength of Compact Shapes
Inelastic Buckling
ppr
pbrppbn M
LL
LLMMMCM
rbp LLL
xyr SFM 7.0
Linear variation between Mp and Mr
Nominal Flexural Strength – Compact Shapes
2
2
2
078.01
ts
b
oxtsb
bcr r
L
hS
Jc
rL
ECF
rbp
brpxcr
ppr
pbrppb
pbp
n LLL
LLMSF
MLL
LLMMMC
LLM
M
for
for
for
Nominal Flexural Strength – NON-Compact Shapes
Most W- M- S- and C- shapes are compact
A few are NON-compact
NONE is slender
Webs of ALL hot rolled shapes in the manual are compactFLB and LTB
Built-Up welded shapes can have non-compact or slender websFLB, WLB, LTB (AISC F4 and F5)