S₁ = 60mm; S₂ = 100mm; S3 = 60mm; S4 = 120mm Thickness of plates (top and bottom): t₁ = 12 mm Thickness of plates (middle): t₂ = 16 mm Steel strength and stresses are: Yield strength, Fy = 250 MPa = 400 MPa Ultimate strength, Fu Allowable tensile stress on the gross area= 0.6Fy Allowable tensile stress on the net area= 0.5Fu Bearing stress on projected area, Fp= 1.5Fu Allowable bolt shear stress, Fv=130 MPa S3 S4 06 T T $1 S2 $1 a) Calculate the allowable tensile load, T (KN) based on tension on the gross area of the plate. b) Calculate the allowable tensile load, T (KN) based on tension on the net area of the plate. Assume the hole diameter is 3 mm more than the bolt diameter. c) Calculate the allowable tensile load, T (KN) based on bolt shear. d) Calculate the allowable tensile load, T (KN) based on tension on the bearing on the projected area of the plate.
S₁ = 60mm; S₂ = 100mm; S3 = 60mm; S4 = 120mm Thickness of plates (top and bottom): t₁ = 12 mm Thickness of plates (middle): t₂ = 16 mm Steel strength and stresses are: Yield strength, Fy = 250 MPa = 400 MPa Ultimate strength, Fu Allowable tensile stress on the gross area= 0.6Fy Allowable tensile stress on the net area= 0.5Fu Bearing stress on projected area, Fp= 1.5Fu Allowable bolt shear stress, Fv=130 MPa S3 S4 06 T T $1 S2 $1 a) Calculate the allowable tensile load, T (KN) based on tension on the gross area of the plate. b) Calculate the allowable tensile load, T (KN) based on tension on the net area of the plate. Assume the hole diameter is 3 mm more than the bolt diameter. c) Calculate the allowable tensile load, T (KN) based on bolt shear. d) Calculate the allowable tensile load, T (KN) based on tension on the bearing on the projected area of the plate.
Steel Design (Activate Learning with these NEW titles from Engineering!)
6th Edition
ISBN:9781337094740
Author:Segui, William T.
Publisher:Segui, William T.
Chapter5: Beams
Section: Chapter Questions
Problem 5.6.3P
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Please answer on the image attached
Thank you
![Refer to the figure. The butt connection shows 8-22mm diameter A325 bolts spaces as follows:
=
S₁ = 60mm; S₂ 100mm; S3 = 60mm; S4 = 120mm
Thickness of plates (top and bottom): t₁ = 12 mm
Thickness of plates (middle): t₂ = 16 mm
Steel strength and stresses are:
Yield strength, Fy = 250 MPa
Ultimate strength, Fu = 400 MPa
Allowable tensile stress on the gross area= 0.6Fy
Allowable tensile stress on the net area= 0.5Fu
Bearing stress on projected area, Fp= 1.5Fu
Allowable bolt shear stress, Fv=130 MPa
Tin
10
S4 S3 S3 S4 S3
+ 6
0 0 0
T
S1
3.
S1
a) Calculate the allowable tensile load, T (KN) based on tension on the gross area of the plate.
b) Calculate the allowable tensile load, T (KN) based on tension on the net area of the plate. Assume
the hole diameter is 3 mm more than the bolt diameter.
c) Calculate the allowable tensile load, T (KN) based on bolt shear.
d) Calculate the allowable tensile load, T (KN) based on tension on the bearing on the projected area of
the plate.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F038f567e-89d0-476b-bc64-2ed6ae6d939b%2F9131c840-b8db-4012-b602-1f73691e6fbd%2Ffrm5ald_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Refer to the figure. The butt connection shows 8-22mm diameter A325 bolts spaces as follows:
=
S₁ = 60mm; S₂ 100mm; S3 = 60mm; S4 = 120mm
Thickness of plates (top and bottom): t₁ = 12 mm
Thickness of plates (middle): t₂ = 16 mm
Steel strength and stresses are:
Yield strength, Fy = 250 MPa
Ultimate strength, Fu = 400 MPa
Allowable tensile stress on the gross area= 0.6Fy
Allowable tensile stress on the net area= 0.5Fu
Bearing stress on projected area, Fp= 1.5Fu
Allowable bolt shear stress, Fv=130 MPa
Tin
10
S4 S3 S3 S4 S3
+ 6
0 0 0
T
S1
3.
S1
a) Calculate the allowable tensile load, T (KN) based on tension on the gross area of the plate.
b) Calculate the allowable tensile load, T (KN) based on tension on the net area of the plate. Assume
the hole diameter is 3 mm more than the bolt diameter.
c) Calculate the allowable tensile load, T (KN) based on bolt shear.
d) Calculate the allowable tensile load, T (KN) based on tension on the bearing on the projected area of
the plate.
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