nzs 3404-1997 example 001

5
Software Verification PROGRAM NAME: ETABS 2013 REVISION NO.: 0 NZS 3404-1997 Example 001 - 1 NZS 3404-1997 Example 001 WIDE FLANGE MEMBER UNDER COMPRESSION EXAMPLE DESCRIPTION The frame object axial strengths are tested in this example. A continuous column is subjected to factored load N = 200 kN. This example was tested using the NZS 3404-1997 steel frame design code. The design capacities are compared with independent hand calculated results. GEOMETRY, PROPERTIES AND LOADING L = 6 m TECHNICAL FEATURES TESTED Section compactness check (compression) Section compression capacity Member compression capacity Material Properties E = 200x10 3 MPa v = 0.3 G = 76923.08 MPa Loading N = 200 kN Design Properties fy = 250 MPa Section: 350WC197 N L A A Section A-A

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Page 1: NZS 3404-1997 Example 001

Software Verification

PROGRAM NAME: ETABS 2013

REVISION NO.: 0

NZS 3404-1997 Example 001 - 1

NZS 3404-1997 Example 001

WIDE FLANGE MEMBER UNDER COMPRESSION

EXAMPLE DESCRIPTION

The frame object axial strengths are tested in this example.

A continuous column is subjected to factored load N = 200 kN. This example

was tested using the NZS 3404-1997 steel frame design code. The design

capacities are compared with independent hand calculated results.

GEOMETRY, PROPERTIES AND LOADING

L = 6 m

TECHNICAL FEATURES TESTED

Section compactness check (compression)

Section compression capacity

Member compression capacity

Material Properties

E = 200x103 MPa

v = 0.3 G = 76923.08 MPa

Loading

N = 200 kN

Design Properties

fy = 250 MPa

Section: 350WC197

N

L

A A

Section A-A

Page 2: NZS 3404-1997 Example 001

Software Verification

PROGRAM NAME: ETABS 2013

REVISION NO.: 0

NZS 3404-1997 Example 001 - 2

RESULTS COMPARISON

Independent results are taken from hand calculations based on the CSI steel

design documentation contained in the file “SFD-NZS-3404-1997.pdf,” which is

available through the program “Help” menu.

Output Parameter ETABS Independent

Percent Difference

Compactness Compact Compact 0.00%

Section Axial Capacity, Ns (kN) 6275 6275 0.00%

Member Axial Capacity, Nc (kN) 4385 4385 0.00%

COMPUTER FILE: NZS 3404-1997 EX001

CONCLUSION

The results show an exact comparison with the independent results.

Page 3: NZS 3404-1997 Example 001

Software Verification

PROGRAM NAME: ETABS 2013

REVISION NO.: 0

NZS 3404-1997 Example 001 - 3

HAND CALCULATION

Properties:

Material:

fy = 250 MPa

Section: 350WC197

Ag = An = 25100 mm2

bf = 350 mm, tf = 28 mm, h = 331 mm, tw = 20 mm

r33 = 139.15 mm, r22 = 89.264 mm

Member:

le33 = le22 = 6000 mm (unbraced length)

Considered to be a braced frame

Loadings:

* 200 kNN

Section Compactness:

Localized Buckling for Flange:

( ) 350 20 2505.89

2 250 2 28 250

f w y

e

f

b t f

t

Flange is under uniform compression, so:

9, 16, 90ep ey ew

5.89 9e ep

, No localized flange buckling

Flange is compact

Page 4: NZS 3404-1997 Example 001

Software Verification

PROGRAM NAME: ETABS 2013

REVISION NO.: 0

NZS 3404-1997 Example 001 - 4

Localized Buckling for Web:

331 25016.55

250 20 250

y

e

w

fh

t

Web is under uniform compression, so:

30, 45, 180ep ey ew

16.55 30e ep

, No localized web buckling

Web is compact.

Section is Compact.

Section Compression Capacity:

Section is not Slender, so Kf = 1.0

31 25,100 250 / 10

s f n yN K A f

6275kNs

N

Member Weak-Axis Compression Capacity:

Frame is considered a braced frame in both directions, so 22 33

1e e

k k

22 33

22 33

6000 600067.216 and 43.119

89.264 139.15

e el l

r r

Buckling will occur on the 22-axis.

22

22

22

1 250600067.216

250 89.264 250

f ye

n

K fl

r

22

22 2

22 22

2100( 13.5)20.363

15.3 2050

n

a

n n

220.5

b since cross-section is not a UB or UC section

Page 5: NZS 3404-1997 Example 001

Software Verification

PROGRAM NAME: ETABS 2013

REVISION NO.: 0

NZS 3404-1997 Example 001 - 5

22 22 22 2267.216 20.363 0.5 77.398

n a b

22 220.00326( 13.5) 0.2083 0

2 2

22

22

22 2 2

22

77.3981 1 0.2083

90 901.317

77.39822

9090

2

22 22

22 22

901 1

c

2

22

901.317 1 1 0.6988

1.317 77.398c

22 22c c s sN N N

220.6988 6275 4385 kN

cN