PSI - Issue 64
Atsushi Sato et al. / Procedia Structural Integrity 64 (2024) 991–998 Author name / Structural Integrity Procedia 00 (2019) 000 – 000
995
5
2
2 2 2 1 32 2 −
16
1
16
e A
e A
1
1
1 − +
1
+
+
+
2
2
2
2
2
W
W
c
N
(
) 2 e c
pl
pl
c
c
(7)
cr
c
=
2
N
y
where e c is the elastic buckling limit of the primary member that is defined as follows: 1 0.6 e c =
(8)
In the range where flexural buckling is not applicable, the following formula will be used to evaluate.
N
(
) 2 e c
(
) 2 c
0.3
c = −
c b −
(9)
cr
c
N
y
where coefficient c is calculated from Eq. (6) where the c → 0 as shown below, and coefficient b is calculated from Eq. (8) where 2 c e c = .
2
2 2 2 1 32 1 −
8
1
8
e A
e A
1
1
1 − +
1
+
+
+
1
2
2
2
W
W
−
c
e A
pl
pl
c
c
lim
1
(10)
c
=
pl = + W
2
0
→
c
Fig. 5 illustrates the proposed strength formula for angle-L150×150×10, c =2.0 with e =14.14mm. The blue line corresponds to Eq. (6); the red line expresses Eqs. (7) and (9) for reinforced members.
Fig. 4. Reinforcement method.
Fig. 5 Proposed strength formulas.
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