unity check examples (asd vs lfrd).pdf
DESCRIPTION
Unity Check Examples (ASD vs LFRD)TRANSCRIPT
![Page 1: Unity Check Examples (ASD vs LFRD).pdf](https://reader035.vdocuments.us/reader035/viewer/2022072922/55cf9c86550346d033aa1fa5/html5/thumbnails/1.jpg)
CE 331, Spring 2007 Example ASD & LRFD Failure Checks 1 / 3
Example problem 1. A simply-supported beam, laterally braced full length.
Dead Load (D) = 2.0 klf
Live Load (L) = 4.0 klf
ftk
ftklfLL
ftkftklfD
D
LwM
LwM
−
−
===
===
5.1128
)15(0.48
3.568
)15(0.28
22
22
Beam is a steel wide flange, W12x53
Yield Stress (Fy) = 50 ksi
S = 70.6 in3
Z = 77.9 in3
Design Method Load Effect Resistance Failure Check
ASD
Allowable Stress Design
ksib
in
inftkftk
b
LD
b
f
f
IyMf
7.218.53
94.4)06.1463.5(4
=
+=
=
−−
+
Fb = 0.66 Fy = 23.8 ksi ksi
ksi
b
b
Ff
8.237.21
= = 0.91 < 1, OK
LRFD
Load and Resistance Factor Design
Mu = 1.2 MD + 1.6 ML
Mu = 1.2 (5.63k-ft) + 1.6 (14.06k-ft)
Mu = 29.3k-ft
φ Mn = (φ) Fy Z
φ Mn = (0.9) 36ksi 12.6in3 / 12 in/ft
φ Mn = 34.0k-ft
ftk
ftk
n
u
MM
−
−
=0.343.29
φ= 0.86 < 1, OK
wD = 2.0 klf wL = 4.0 klf
15 ft
strength reduction factor
allowable bending stress
unity check
factored moment nominal moment capacity
![Page 2: Unity Check Examples (ASD vs LFRD).pdf](https://reader035.vdocuments.us/reader035/viewer/2022072922/55cf9c86550346d033aa1fa5/html5/thumbnails/2.jpg)
CE 331, Spring 2007 Example ASD & LRFD Failure Checks 2 / 3
Example problem 2. A simply-supported beam, laterally braced full length.
Dead Load (D) = 2.0 klf Live Load (L) = 4.0 klf
ftkftklfL
L
ftkftklfD
D
LwM
LwM
−
−
===
===
5.1128
)15(0.48
3.568
)15(0.28
22
22
Beam is a steel wide flange, W12x53
Yield Stress (Fy) = 50 ksi
S = 70.6 in3
Z = 77.9 in3
Design Method Load Effect Resistance Failure Check
ASD
Allowable Stress Design ksi
ftinftkftk
b
LD
b
inf
SMf
7.286.70
12)5.1123.56(3
/
=+
=
=
−−
+Lc = 9.0ft, Lu = 15.9ft (p 132 FE Ref)
Lc < (Lb = 15ft ) < Lu ∴Fb = 0.60 Fy = 0.6 (50ksi) Fb = 30ksi
ksi
ksi
b
b
Ff
307.28
= = 0.96 < 1
OK
LRFD
Load and Resistance Factor Design
Mu = 1.2 MD + 1.6 ML
Mu = 1.2 (56.3k-ft) + 1.6 (112.5k-ft)
Mu = 248k-ft
Lp = 8.8ft, Lr = 25.6ft (p 128 FE Ref) Lp < (Lb = 15ft) < Lr ∴φ Mn = Cb [φ Mp – BF(Lb – Lp)] < φ Mp Cb = 1.0 (always for this class) φ Mp = 292k-ft (p 128 FE Ref) BF = 4.78k (p 128 FE Ref) φ Mn = (1) [292kpft – (4.78k(15ft – 8.8ft)] φ Mn = 262k-ft (< 292k-ft = φ Mp)
ftk
ftk
n
u
MM
−
−
=262248
φ= 0.95 < 1
OK
wD wL
15 ft
unbraced length of compression flange
section modulus = I / y
![Page 3: Unity Check Examples (ASD vs LFRD).pdf](https://reader035.vdocuments.us/reader035/viewer/2022072922/55cf9c86550346d033aa1fa5/html5/thumbnails/3.jpg)
CE 331, Spring 2007 Example ASD & LRFD Failure Checks 3 / 3
Example problem 3. A single column, laterally braced at mid-height for buckling in the weak direction, no lateral support for buckling in the strong direction.
Dead Load (D) = 25k
Live Load (L) = 75k
Beam is a steel wide flange, W6x20 Yield Stress (Fy) = 50 ksi Ixx = 41.4 in4
Iyy = 13.3 in4 A = 5.87 in2
Lu_x = 18 ft (unbraced length for buckling in the strong direction)
Lu_y = 9 ft (unbraced length for buckling in the weak direction)
Design Method
Load Effect Resistance Failure Check
ASD
ksia
kkLD
a
f
inAPf
0.17
87.57525
2
=
+==
+
0.7250.1
)1
129)(0.1(
5.8165.2
)1
1218)(0.1(
50.187.53.13
65.287.5
1.41
_
_
2
4
2
4
==
==
===
===
in
ft
inft
y
yuy
in
ft
inft
x
xux
inyy
inxx
rLk
rLk
inin
AI
r
inin
AIr
Fa = 18.7ksi [ from Table on pg 134 FE Ref. for Fy = 50ksi and kL/r = 81.5 ]
ksi
ksi
a
a
Ff
7.180.17
= = 0.91 < 1,
OK
LRFD
Pu = 1.2 PD + 1.6 PL
Pu = 1.2 (25k) + 1.6 (75k)
Pu = 150k Ref.) FE131 p (Table 16.26
above) from(5.81max
ksicrcF
rLk
=
=⎟⎠⎞
⎜⎝⎛
φ
φcFcr = 26.16ksi [from Table on pg 131 FE Ref. for Fy = 50ksi and kL/r = 81.5 ]
φ Pn = φc Fcr A = 26.2ksi 5.87in2
φ Pn =153.8kt
k
k
n
u
PP
8.153150
=φ
= 0.98 < 1,
OK
PD = 25k
9 ft
PL = 75k
9 ft
unity check
allowable axial stress
slenderness ratio controls
factored axial force
nominal axial capacity