Contents AISC 360 10 Example 001

User Manual: AISC-360-10 Example 001

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Software Verification
PROGRAM NAME:
REVISION NO.:

ETABS
0

AISC-360-10 Example 001
COMPOSITE COLUMN DESIGN
EXAMPLE DESCRIPTION
Determine if the 14-ft.-long filled composite member illustrated below is
adequate for the indicated dead and live loads. The composite member consists
of an ASTM A500 Grade B HSS with normal weight (145 lb/ft3) concrete fill
having a specified compressive strength, fc′ = 5 ksi.
GEOMETRY, PROPERTIES AND LOADING

Member Properties
HSS10x6 x⅜
E = 29,000 ksi
Fy = 46 ksi

Loading
PD = 32.0 kips
PL = 84.0 kips

Geometry
Height, L = 14 ft

AISC-360-10 Example 001 - 1

Software Verification
PROGRAM NAME:
REVISION NO.:

ETABS
0

TECHNICAL FEATURE OF ETABS TESTED
Compression capacity of composite column design.
RESULTS COMPARISON
Independent results are referenced from Example I.4 from the AISC Design
Examples, Version 14.0.
ETABS

Independent

Percent
Difference

Required Strength Pu (kip)

172.8

172.8

0.00%

Available Strength ΦPn (kip)

342.93

354.78

3.34%

Output Parameter

COMPUTER FILE: AISC-360-10 EXAMPLE 001.EDB
CONCLUSION
The ETABS results show an acceptable comparison with the independent results.

AISC-360-10 Example 001 - 2

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ETABS
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HAND CALCULATION
Properties:
Materials:
ASTM A500 Grade B Steel
E = 29,000 ksi, Fy = 46 ksi, Fu = 58 ksi
5000 psi normal weight concrete
Ec = 3,900 ksi, f c′ = 5 ksi, wconcrete = 145 pcf
Section dimensions and properties:
HSS10x6x⅜
H = 10.0 in, B= 6.00 in, t = 0.349 in
As = 10.4 in2, Isx = 137 in4, Isy = 61.8 in4
Concrete area

hi = H − 2 • t = 10 − 2 • 0.349 = 9.30 in.

bi = B − 2 • t = 6 − 2 • 0.349 = 5.30 in.
Ac= bi • hi − t 2 • (4 − π)= 5.30 • 9.30 − (0.349) 2 • (4 − π)= 49.2 in.2

Moment of inertia for bending about the y-y axis:
( H − 4 • t ) • bt3 t • ( B − 4 • t )3 (9π2 − 64) • t 4
 B − 4•t 4•t 
=
+
+
+ π • t2 
−
I cy

12
6
36 • π
2
3• π 


2

(10 − 4 • 0.349) • 5.303 0.349 • (6 − 4 • 0.349)3 (9π2 − 64) • 0.3494
+
+
+
12
6
36 • π
6 − 4 • 0.349 4 • 0.349 2
)
π • 0.3492 (
−
2
3• π
= 114.3 in.4

=

Design for Compression:
Required Compressive Strength:

Pu = 1.2 • PD + 1.6 • PL = 1.2 • 32.0 + 1.6 • 84.0 = 172.8 kips

AISC-360-10 Example 001 - 3

Software Verification
PROGRAM NAME:
REVISION NO.:

ETABS
0

Nominal Compressive Strength:

E 
Pno = Pp = Fy • As + C2 • f c′  Ac + Asr s 
Ec 

where

C2 = 0.85 for rectangular sections

Asr = 0 when no reinforcing is present within the HSS
Pno = 46 • 10.4 + 0.85 • 5 • (49.2 + 0.0) = 687.5 kips
Weak-axis Elastic Buckling Force:
 As 
0.6 + 2 
C3 =
 ≤ 0.9
 Ac + As 
 10.4 
=
0.6 + 2 
 ≤ 0.9
 49.2 + 10.4 
0.9 controls
= 0.949 > 0.9

EI eff = Es • I sy + Es • I sr + C3 • Ec • I cy
= 29, 000 • 62.1 + 0 + 0.9 • 3,900 • 114.3
= 2, 201, 000 kip-in 2
Pe = π2 ( EI eff ) ( KL) 2 where K = 1.0 for a pin-ended member
=
Pe

π2 • 2, 201, 000
= 769.7 kips
1.0 • (14.0 • 12) 2

Available Compressive Strength:
Pno
688
=
= 0.893 < 2.25
Pe 769.7

Therefore, use AISC Specification Equation I2-2:
Pno


ΦPn =
ΦPno 0.658 Pe  =
0.75 • 687.5 • (0.658)0.893 =
354.8 kips



AISC-360-10 Example 001 - 4



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