1. Calculate the critical slenderness ratio of the member. A. 26.208 B. 45.882 C. 36.706 D.27.529 2. Calculate the nominal axial load capacity of the column. A. 3 104 kN B. 4 851 KN C. 4 213 KN D.5 344 KN 3. Calculate the service axial dead load if the service axial live load is twice as that of the dead load. Use LRFD. A. 1 354 KN B. 992 KN C. 1 093 KN D.634 KN
1. Calculate the critical slenderness ratio of the member. A. 26.208 B. 45.882 C. 36.706 D.27.529 2. Calculate the nominal axial load capacity of the column. A. 3 104 kN B. 4 851 KN C. 4 213 KN D.5 344 KN 3. Calculate the service axial dead load if the service axial live load is twice as that of the dead load. Use LRFD. A. 1 354 KN B. 992 KN C. 1 093 KN D.634 KN
Steel Design (Activate Learning with these NEW titles from Engineering!)
6th Edition
ISBN:9781337094740
Author:Segui, William T.
Publisher:Segui, William T.
Chapter10: Plate Girders
Section: Chapter Questions
Problem 10.7.9P
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
Transcribed Image Text:13
NSCP 2015
Pn = FerAg
(505.3-1)
The flexural buckling stress, Fer, is determined as follows:
KL
1. when
r
1.71 (or F, 2 0.44F,)
(or F. 2 0.44F,)
Fy
Fr = 0.
Fy
(505.3-2)
KL
E
> 4.71
Fy
( or F. < 0.44F,)
2.
when
r
Fer = 0.877F.
(505.3-3)
where
F.= elastic critical buckling stress determined according
to Eq. 505.3-4, Section 505.4, or the provisions of
Section 503.2, as applicable, MPa.
F =
KL
(505.3-4)
A W12x79 of A573 Grade 60 (Fy = 415 MPa) steel is used as a compression
member. It is 7 m long, fixed at the top and bottom, and has additional support in
the weak direction 3 m from the top. Properties of the section are: A = 14,500
mm2 , I = 258.6 x 10° mm“, Iy = 84.375 x 10° mmª
1.
Calculate the critical slenderness ratio of the member.
А. 26.208
C. 36.706
B. 45.882
D. 27.529
2.
Calculate the nominal axial load capacity of the column.
B. 4 851 kN
A. 3 104 kN
C. 4 213 kN
D.5 344 kN
3.
Calculate the service axial dead load if the service axial live load is twice as
that of the dead load. Use LRFD.
A. 1 354 kN
C. 1 093 kN
B. 992 kN
D.634 kN
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