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SteelChk - Strut (Rev. D) 20190508

The document summarizes the structural design of a primary strut made of 254 x 254 x 73 UC Grade 43 hot-rolled steel. Key details include: - The strut is designed to withstand a maximum inclined prop load of 36 kN/m and maximum compression force of 72 kN. - The section is classified as compact. - Design checks are performed for bending moment, shear force, and axial force to ensure the strut meets the required load capacities.

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100% found this document useful (1 vote)
423 views5 pages

SteelChk - Strut (Rev. D) 20190508

The document summarizes the structural design of a primary strut made of 254 x 254 x 73 UC Grade 43 hot-rolled steel. Key details include: - The strut is designed to withstand a maximum inclined prop load of 36 kN/m and maximum compression force of 72 kN. - The section is classified as compact. - Design checks are performed for bending moment, shear force, and axial force to ensure the strut meets the required load capacities.

Uploaded by

hessian123
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
You are on page 1/ 5

#N/A Job No.

:
By:
ELS Design Chkd:
Primary Strut Checking Date: 8-May-19

Structural Steel Design - Primary Strut


(Structural steel design based on "Code of Practice for the Structural Use of Steel 2005"
with reference to "The Design and Construction of Sheet-Piled Cofferdams by B P Williams and D Waite")

Plan
Primary Strut

Secondary Strut
Waling

S/2 S S/2
Section

Strut B y
y T
q
t

D x x x
x d

y T y
Wall a

1. Section Properties

Try Section : Single 254 x 254 x 73 UC Grade 43 Hot Rolled

Distance between centre line a = 0 mm Neglect Spacing


Depth of Section D = 254 mm Elastic Modulus (X-Axis) Zx = 894000 mm3
Width of Section B = 254 mm Elastic Modulus (Y-Axis) Zy = 304724 mm3
Web Thickness t = 8.6 mm Plastic Modulus (X-Axis) Sx = 989000 mm
3

Flange Thickness T = 14.2 mm Plastic Modulus (Y-Axis) Sy = 462000 mm3


Depth between Fillets d = 200.3 mm Buckling Parameter u = 0.849
Second Moment of Area (X-Axis) Ix = 114000000 mm
4
Torsional Index x = 17.3
Second Moment of Area (Y-Axis) Iy = 38700000 mm
4
Area of Section Ag = 9290 mm2
Radius of Gyration (X-Axis) rx = 111.0 mm Mass per Length w = 73.00 kg/m
2
Radius of Gyration (Y-Axis) ry = 64.54 mm Design Strength py = 275 N/mm
The Modulus of Elasticity for steel E = 205000.00 MPa

2. Ultimate Design Load

Maximum inclined prop load from Plaxis = 36.00 kN/m


Stiffness of Strut for Plaxis Input, EA = (205,000 x 10^3) x (9,290 / 10^6) /2 = 9.522E+05 kN/m
Maximum prop force, F = 36.00 kN/m
Minimum inclination of strut to waling, a = 90.00 degree
Load in the direction of strut, Pa = F / sin a = 36.00 / sin 90.0 = 36.0 kN/m
Maximum strut spacing, S = 2.00 m
Maximum compression, P = Pa x S = 36.00 x 2.00 = 72.0 kN
Inclination of strut to wall, q = 90.00 degree
Unrestrain length of strut on plan (X-Axis), Lx' = 2.00 m
Actual unrestrain length of strut (X-Axis), Lx = Lx' / sin q = 2.00 / sin 90.0 = 2.00 m
Unrestrain length of strut on plan (Y-Axis), Ly' = 2.00 m
Actual unrestrain length of strut (Y-Axis), Ly = Ly' / sin q = 2.00 / sin 90.0 = 2.00 m
Construction Load, Qc = 0.00 kPa
Maximum Bending Moment (unfactored) = 0.125 x (73.0 x 9.81 + 0.0 x 254.0 x 1) x 10^-3 x 2.0^2 = 0.4 kNm
Maximum Shear Force (unfactored) = 0.5 x (73.0 x 9.81 +0.0 x 254.0 x 1) x 10^-3 x 2.0 = 0.7 kN
Load Factor = 1.60
spacing 1
Design Bending Moment (X-Axis) Mx = 160.0 kNm Design Shear Force V = 120.0 kN
Design Bending Moment (Y-Axis) My = 0.0 kNm Axial Force Fc = 115.2 kN

3. Section Classification (Table 7.1)

ε = [275 / py]1/2 = 1.0 b/T = 8.9 < 9.0 ε (Compact) (Table 7.1, Outstand element of compression flange)
d/t = 23.3 < 80 ε (Plastic) (Table 7.1, Web with neutral axis at mid-depth)

Class of Section = Compact Section

Primary Strut, SteelChk - Strut (Rev. D) 20190508


#N/A Job No.:
By:
ELS Design Chkd:
Primary Strut Checking Date: 8-May-19

4. Shear Buckling Resistance (Clause 8.4.6)

d/t = 23.3 < 70ε = 70.0

Therefore, Not Required to Check for Shear Buckling

5. Check Shear Capacity (Clause 8.2.1)

Shear Area Av = 2184 mm2


Shear Capacity Vc = pyAv/(3)^0.5
= 347 kN
Design Shear Force V = 120.0 kN < Pv = 347 kN Check Shear OK

Since, 0.6Vc = 208 kN > V Low Shear

7. Check Lateral Torsional Buckling (Clause 8.3)

Unrestrain length (Y-Axis) Ly = 2.00 m


Effective Length LEy = 1.0 L = 2.0 m (Clause 8.3.4)
Minor Axis Slenderness l = LEy / ry = 31.0
Buckling parameter u = 0.85 (Clause 8.3.5.3)
l/x = 1.79
2 0.25
Slenderness factor n = 1/(1+0.05(l/x) ) (Clause 8.3.5.3 Eqn 8.27)
= 0.963
bw = 1.000 (Clause 8.3.5.3 Eqn 8.28, 8.29)
l LT
0.5
Equivalent Slenderness = uvl(b w) = 25.3 (Clause 8.3.5.3 Eqn 8.25)

Design strength py = 275.00 N/mm2


Buckling strength pb = 275.0 N/mm2 (Table 8.3a for rolled section)
Buckling resistance moment Mb = 272.0 kNm (Clause 8.3.5.2 Eqn 8.20, 8.21, 8.22, 8.23, 8.24)

Equivalent uniform moment factor mLT = 0.93 (Table 8.4a for no intermediate lateral restraint)

mLTMx = 148.80 < Mb= 272.0 kNm (Clause 8.3.5.2 Eqn 8.18)
and Mx = 160.00 < Mcx= 272.0 kNm (Clause 8.3.5.2 Eqn 8.19)
Lateral Torsional Buckling Resistance OK

8. Cross-section Capacity Check (Clause 8.9.1)

Fc Mx My 115.2 160.0 0.0


+ + = + +
Agpy Mcx Mcy 2554.8 272.0 100.6

= 0.05 + 0.59 + 0.00


= 0.63
< 1 Cross-section Capacity OK

Primary Strut, SteelChk - Strut (Rev. D) 20190508


#N/A Job No.:
By:
ELS Design Chkd:
Primary Strut Checking Date: 8-May-19

9. Member Buckling Resistance Check (Clause 8.9.2)

Axis of buckling = x-x


Unrestrain length (X-Axis) Lx = 2.00 m
Effective Length (X-Axis) LEx = 1.0 Lx = 2.00 m (Clause 8.3.4)
Major Axis Slenderness lx = LEx / rx = 18.0 ≈ 20
Maximum Thickness T = 14.2 mm ≤ 40 mm
Type of Section = Rolled H-section ≤ 40mm
Designation of buckling curves for different section types: Buckling Curve b) (Table 8.7)
2
Compressive Strength pcx = 272.00 N/mm (Table 8.8(b))

Axis of buckling = y-y


Unrestrain length (Y-Axis) Ly = 2.00 m
Effective Length (Y-Axis) LEy = 1.0 Ly = 2.00 m (Clause 8.3.4)
Minor Axis Slenderness ly = LEy / ry = 31.0 ≈ 35
Maximum Thickness T = 14.2 mm ≤ 40 mm
Type of Section = Rolled H-section ≤ 40mm
Designation of buckling curves for different section types: Buckling Curve c) (Table 8.7)
2
Compressive Strength pcy = 247.00 N/mm (Table 8.8(c))

Design Compressive Strength pc = min. of pcx & pcy = 247.0 N/mm2


Moment equivalent factor m for flexural buckling
mx = 0.95 (Table 8.9)
my = 0.95 (Table 8.9)

Amplication Factor
fx = 1.00
fy = 1.01
Axis of buckling = x-x
Unrestrain length (X-Axis) Lx = 2.00 m
Effective Length (X-Axis) LEx = 1.0 Lx = 2.00 m (Clause 8.3.4)
Major Axis Slenderness lx = LEx / rx = 18.0 ≈ 20
Maximum Thickness T = 14.2 mm ≤ 40 mm
Type of Section = Rolled H-section ≤ 40mm
Designation of buckling curves for different section types: Buckling Curve b) (Table 8.7)

Primary Strut, SteelChk - Strut (Rev. D) 20190508


#N/A Job No.:
By:
ELS Design Chkd:
Primary Strut Checking Date: 8-May-19

Compressive Strength pcx = 272.00 N/mm2 (Table 8.8(b))

Axis of buckling = y-y


Unrestrain length (Y-Axis) Ly = 2.00 m
Effective Length (Y-Axis) LEy = 1.0 Ly = 2.00 m (Clause 8.3.4)
Minor Axis Slenderness ly = LEy / ry = 31.0 ≈ 35
Maximum Thickness T = 14.2 mm ≤ 40 mm
Type of Section = Rolled H-section ≤ 40mm
Designation of buckling curves for different section types: Buckling Curve c) (Table 8.7)
2
Compressive Strength pcy = 247.00 N/mm (Table 8.8(c))

2
Design Compressive Strength pc = min. of pcx & pcy = 247.0 N/mm

Cross-section capacity
Fc mxMx myMy 115.2 160.0 0.0
+ + = + + (Clause 8.9.1 Eqn 8.78)
Agpc Mcx Mcy 2554.8 272.0 100.6

= 0.05 + 0.59 + 0.00


= 0.63
< 1 Overall Capacity OK

Member buckling resistance


Fc mxMx myMy 0.0 152.0 0.0
+ + = + + (Clause 8.9.2 Eqn 8.79)
Agpc Mcx Mcy 2294.6 272.0 100.6

= 0.00 + 0.56 + 0.00


= 0.56
< 1 Overall Capacity OK

Fc mxMx myMy 0.0 152.3 0.0


+ + = + + (Clause 8.9.2 Eqn 8.80)
Agpc Mcx Mcy 2294.6 272.0 100.6

= 0.00 + 0.56 + 0.00


= 0.56
< 1 Overall Capacity OK

Fc mxMx myMy 0.0 148.8 0.0


+ + = + + (Clause 8.9.2 Eqn 8.81)
Agpc Mcx Mcy 2294.6 272.0 100.6

= 0.00 + 0.55 + 0.00


= 0.55
< 1 Overall Capacity OK

10. Check Welding Connection between the Strut and Waling

Axial Force Fc = 115.2 kN


Minimum inclination of strut to waling a = 88.00 degree (Refer to P.1 drawing)
Inclination of strut to wall q = 88.00 degree (Refer to P.1 drawing)

Mass per Length Span Length Width of Section Factored Self-weight Factored Construction load
Structural Members w (kg/m) L (m) B (mm) (kN) (kN)
Design Strut 73.0 2.00 254.0 1.15 0.00
Connected Strut 1 0.0 0.00 0.0 0.00 0.00
Connected Strut 2 0.0 0.00 0.0 0.00 0.00
Total 1.15 0.00

Horizontal Shear Force FH = Fc cosa = 4.0 kN


Vertical Shear Force FV = Fc cosq + Self-weight + Construction load
= 5.17 kN
Total Shear Force Induced by Strut V = (FH2 + FV2)0.5
= 6.5 kN

Provide 6 mm fillet weld at Flange Max. Thickness = 12.2 mm (Clause 9.2.5.1.2a)


Provide 6 mm fillet weld at Web Max. Thickness = 6.6 mm Thickness OK

Design Strength of fillet weld pw = 220 N/mm2 (Table 9.2a)

Weld at Flange
Leg Length s = 6 mm
Throat Size a = 0.7 s = 4.2 mm
Weld Shear Capacity per unit Length PL = pw a = 0.924 kN/mm (Clause 9.2.5.1.6 Eqn 9.4)
Weld Length L = 4B - 2t + 4T = 1055.6 mm
Weld Shear Strength Provided PL L = 975.4 kN

Primary Strut, SteelChk - Strut (Rev. D) 20190508


#N/A Job No.:
By:
ELS Design Chkd:
Primary Strut Checking Date: 8-May-19

Weld at Web
Leg Length s = 6 mm
Throat Size a = 0.7 s = 4.2 mm
Weld Shear Capacity per unit Length PL = pw a = 0.924 kN/mm (Clause 9.2.5.1.6 Eqn 9.4)
Weld Length L = 2D - 4T = 451.2 mm
Weld Shear Strength Provided PL L = 416.9 kN

Total Weld Shear Strength Provided = 975.4 + 416.9


= 1392.3 kN > V= 6.5 kN Welding Connection OK

Primary Strut, SteelChk - Strut (Rev. D) 20190508

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