Civil Engineering Reference
In-Depth Information
Therefore,
1.33 ( 771.2 )
1.208 ( 557.2 )
98.1 ( E80 ) =
LLT
=
1.39 ( E80 ) =
E111.
P 1 max =+
54.56
+
1.208 ( +
332.4 )( 122 / 80 ) =
666.4 kips.
Strength considerations:
456.1
0.55 ( 50 )
16.6 in. 2 (tensile yielding)
A g
456.1
0.47 ( 70 )
13.9 in. 2 (fracture)
A e
due to strength-related shear lag effects at the connection (assuming U c =
0.90)
13.9
U c
15.4 in. 2 (fracture)
A e
from the requirement related to live load LLT
611.7
1.33 ( 0.55 )( 50 )
16.7 in. 2 (tensile yielding)
A g
611.7
1.33 ( 0.47 )( 70 )
14.0 in. 2 (fracture)
A e
due to strength-related shear lag effects of LLT at the connection
14.0
U c =
15.6 in. 2 (fracture).
A e
Fatigue considerations:
A efat ( 385.7 / 16 )
24.1 in. 2 for the gross area of connected elements of
the member
A e ( 385.7/24 )
16.1 in. 2 for the net area of the member away from the
connection.
Stiffness considerations:
L
r min
200
( 27.25 ) 2
+ ( 19.55 ) 2 ( 12 )
r min
2.01 in.
200
Select a member with the following section properties:
Minimum gross area of the member
18.2 in. 2 (tensile yielding)
Minimum gross area for portions of the member connected
=
A g
A g
=
24.1 in. 2 (fatigue)
Minimum net effective area of the member at the connection
=
A e
15.6 in. 2 (fracture)
Minimum net area of the member away from the connection
=
A e
16.1 in. 2 (fatigue)
Minimum radius of gyration
=
r min
2.01 in.
 
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