D11.A.7 Output Format
Results of code checking and member selection are presented in a tabular format. The term CRITICAL COND refers to the section of the NZS3404 specification which governs the design.
D11.A.7.1 TRACK 0
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|* PMemberPMEMBER for physical member, MEMBER for analytical member Number: 1 |
| Member Section: ST PFC250 (AISC SECTIONS) |
| Status: FAIL Ratio: 4.381 Critical Load Case: 1 Location: 0.42 |
| Critical Condition: Cl.5.1 |
| Critical Design Forces: (Unit: KN METE) |
| FX: 4.448E+00 C FY: 0.000E+00 FZ: 43.563E+00 |
| MX: 0.000E+00 MY: 0.000E+00 MZ: 0.000E+00 |
|----------------------------------------------------------------------------------|
D11.A.7.2 TRACK 1
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|* PMemberPMEMBER for physical member, MEMBER for analytical member Number: 1 |
| Member Section: ST PFC250 (AISC SECTIONS) |
| Status: FAIL Ratio: 4.381 Critical Load Case: 1 Location: 0.42 |
| Critical Condition: Cl.5.1 |
| Critical Design Forces: (Unit: KN METE) |
| FX: 4.448E+00 C FY: 0.000E+00 FZ: 43.563E+00 |
| MX: 0.000E+00 MY: 0.000E+00 MZ: 0.000E+00 |
|----------------------------------------------------------------------------------|
| ϕMsz = 113.670E+00 KNm ϕMsy = 24.010E+00 KNm [Cl.5.1 ] |
| ϕMbz = 43.939E+00 KNm [Cl.5.1 ] |
| ϕVvy = 324.000E+00 KNm ϕVvz = 437.400E+00 KNm [Cl.5.12.3 ] |
| ϕNs = 1.220E+03 KN [Cl.6.1 ] |
| ϕNcz = 601.788E+00 KN ϕNcy = 74.742E+00 KN [Cl.6.1 ] |
| ϕNt = 1.220E+03 KN [Cl.7.1 ] |
| ϕMrz = 113.670E+00 KNm ϕMry = 24.010E+00 KNm [Cl.8.3.2 ] |
| ϕMiz = 113.670E+00 KNm ϕMiy = 24.010E+00 KNm [Cl.5.3.2.4] |
| ϕMozc = 0.000E+00 KNm ϕMozt = 0.000E+00 KNm [ ] |
| ϕMcz = 0.000E+00 KNm [ ] |
| ϕMtz = 0.000E+00 KNm [ ] |
|----------------------------------------------------------------------------------|
D11.A.7.3 TRACK 2
STAAD.PRO CODE CHECKING - NZS-3404-1997 (v1.0)
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MEMBER DESIGN OUTPUT FOR PMEMBERPMEMBER for physical member, MEMBER for analytical member 1
DESIGN Notes
------------
1. (*) next to a Load Case number signifies that a P-Delta analysis has not been performed for
that particular Load Case; i.e. analysis does not include second-order effects.
2. ϕ = 0.9 for all the calculations [NZS3404 Table 3.4]
3. (#) next to Young's modulus E indicates that its value is not 200000 MPa as per NZS3404 1.4.
DESIGN SUMMARY
--------------
Designation: ST PFC250 (AISC SECTIONS)
Governing Load Case: 1*
Governing Criteria: Cl.5.1
Governing Ratio: 4.381 *(FAIL)
Governing Location: 4.500 m from Start.
SECTION PROPERTIES
------------------
d: 250.0000 mm bf: 90.0000 mm
tf: 15.0000 mm tw: 8.0000 mm
Ag: 4520.0000 mm2 J: 238.0000E+03 mm4 Iw: 34.8250E+09 mm6
Iz: 45.1000E+06 mm4 Sz: 421.0000E+03 mm3 (plastic) Zz: 360.8000E+03 mm3 (elastic)
rz: 99.8893E+00 mm
Iy: 3.6400E+06 mm4 Sy: 107.0000E+03 mm3 (plastic) Zy: 59.2834E+03 mm3 (elastic)
ry: 28.3780E+00 mm
STAAD SPACE -- PAGE NO. 9
MATERIAL PROPERTIES
-------------------
Material Standard : AS/NZS 3679.1
Nominal Grade : 300
Residual Stress Category : HR (Hot-rolled)
E (#) : 204999.984 MPa [NZS3404 1.4]
G : 80000.000 MPa [NZS3404 1.4]
fy, flange : 300.000 MPa [NZS3404 Table 2.1]
fy, web : 320.000 MPa [NZS3404 Table 2.1]
fu : 440.000 MPa [NZS3404 Table 2.1]
BENDING
-------
Section Bending Capacity (about Z-axis)
Critical Load Case : 1*
Critical Ratio : 1.694
Critical Location : 4.500 m from Start.
Mz* = -192.5156E+00 KNm
Section Slenderness: Compact
Zez = 421.0000E+03 mm3
ϕMsz = 113.6700E+00 KNm [NZS3404 Cl.5.1 ]
Section Bending Capacity (about Y-axis)
Critical Load Case : 1*
Critical Ratio : 0.000
Critical Location : 0.000 m from Start.
My* = 0.0000E+00 KNm
Section Slenderness: Compact
Zey = 88.9251E+03 mm3
ϕMsy = 24.0098E+00 KNm [NZS3404 Cl.5.1 ]
Member Bending Capacity
Critical Load Case : 1*
Critical Ratio : 4.381
Critical Location : 4.500 m from Start.
Crtiical Flange Segment:
Location (Type): 0.00 m(F )- 9.00 m(F )
Mz* = -192.5156E+00 KNm
kt = 1.00 [NZS3404 Table 5.6.3(1)]
kl = 1.00 [NZS3404 Table 5.6.3(2)]
kr = 1.00 [NZS3404 Table 5.6.3(3)]
le = 9.00 m [NZS3404 5.6.3]
αm = 1.384 [NZS3404 5.6.1.1.1(b)(iii)]
Mo = 42.2526E+00 KNm [NZS3404 5.6.1.1.1(d)]
αsz = 0.279 [NZS3404 5.6.1.1.1(c)]
ϕMbz = 43.9390E+00 KNm (<= ϕMsz) [NZS3404 5.6.1.1.1(a)]
STAAD SPACE -- PAGE NO. 10
SHEAR
-----
Section Shear Capacity (along Y-axis)
Critical Load Case : 1*
Critical Ratio : 0.134
Critical Location : 0.000 m from Start.
Vy* = 43.5625E-03 KN
ϕVvy = 324.0000E-03 KN [NZS3404 5.11.2]
Section Shear Capacity (along Z-axis)
Critical Load Case : 1*
Critical Ratio : 0.000
Critical Location : 0.000 m from Start.
Vz* = 0.0000E+00 KN
ϕVvz = 437.4000E-03 KN [NZS3404 5.11.2]
STAAD SPACE -- PAGE NO. 11
AXIAL
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Section Compression Capacity
Critical Load Case : 1*
Critical Ratio : 0.000
Critical Location : 0.000 m from Start.
N* = 0.0000E+00 KN
Ae = 4.5200E+03 mm2 [NZS3404 6.2.3 / 6.2.4]
kf = 1.000 [AS 4100 6.2.2]
An = 4.5200E+03 mm2
ϕNs = 1.2204E+03 KN [NZS3404 6.2.1]
Member Compression Capacity (about Z-axis)
Critical Load Case : 1*
Critical Ratio : 0.000
Critical Location : 0.000 m from Start.
N* = 0.0000E+00 KN
Unbraced Segment:
Location (Type): 0.00 m(U )- 9.00 m(U )
Lez = 9.00 m
αb = 0.50 [NZS3404 Table 6.3.3(1)/6.3.3(2)]
λn,z = 98.699 [NZS3404 6.3.3]
λ,z = 107.400 [NZS3404 6.3.3]
ε,z = 0.959 [NZS3404 6.3.3]
αc,z = 0.493 [NZS3404 6.3.3]
ϕNcz = 0.6018E+3 KN [NZS3404 6.3.3]
Member Compression Capacity (about Y-axis)
Critical Load Case : 1*
Critical Ratio : 0.000
Critical Location : 0.000 m from Start.
N* = 0.0000E+00 KN
Unbraced Segment:
Location (Type): 0.00 m(U )- 9.00 m(U )
Ley = 9.00 m
λn,y = 347.417 [NZS3404 6.3.3]
λ,y = 350.403 [NZS3404 6.3.3]
ε,y = 0.569 [NZS3404 6.3.3]
αc,y = 0.061 [NZS3404 6.3.3]
ϕNcy = 0.7474E+2 KN [NZS3404 6.3.3]
Section Tension Capacity
Critical Load Case : 1*
Critical Ratio : 0.000
Critical Location : 0.000 m from Start.
N* = 0.0000E+00 KN
kt = 0.00 [User defined]
An = 4.5200E+03 mm2
ϕNt = 1.2204E+03 KN [NZS3404 7.2]
STAAD SPACE -- PAGE NO. 12
COMBINED BENDING AND AXIAL
------------------------
Section Combined Capacity (about Z-axis)
Critical Load Case : 1*
Critical Ratio : 1.694
Critical Location : 4.500 m from Start.
ϕMrz = 113.6700E+00 KNm [NZS3404 8.3.2]
Section Combined Capacity (about Y-axis)
Critical Load Case : 1*
Critical Ratio : 0.000
Critical Location : 0.000 m from Start.
ϕMry = 24.0098E+00 KNm [NZS3404 8.3.3]
Section Combined Capacity (Biaxial)
Critical Load Case : 1*
Critical Ratio : 1.694
Critical Location : 4.500 m from Start.
γ = 1.400 [NZS3404 8.3.4]
Member In-plane Capacity (about Z-axis)
Critical Load Case : 1*
Critical Ratio : 1.694
Critical Location : 4.500 m from Start.
ϕMiz = 113.6700E+00 KNm [NZS3404 8.4.2]
Member In-plane Capacity (about Y-axis)
Critical Load Case : 1*
Critical Ratio : 0.000
Critical Location : 0.000 m from Start.
ϕMiy = 24.0098E+00 KNm [NZS3404 8.4.2]
Member Out-of-plane Capacity (Tension)
Critical Load Case : 1*
Critical Ratio : 0.000
Critical Location : 0.000 m from Start.
αbc = 0.00
ϕNoz = 0.0000E+00 KN [NZS3404 8.4.4.1.2]
ϕMoz,t= 0.0000E+00 KNm [NZS3404 8.4.4.1]
Member Out-of-plane Capacity (Compression)
Critical Load Case : 1*
Critical Ratio : 0.000
Critical Location : 0.000 m from Start.
ϕMoz,c= 0.0000E+00 KNm [NZS3404 8.4.4.2]
Member Biaxial Capacity (Tension)
Critical Load Case : 1*
Critical Ratio : 0.000
Critical Location : 0.000 m from Start.
Member Biaxial Capacity (Compression)
Critical Load Case : 1*
Critical Ratio : 0.000
Critical Location : 0.000 m from Start.
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