18
B 4
B 4
B
2
b
b
d
B
2
h H
h
B
(approx)
I = l
12
B
2
I = + +
t
4
t
2
3
3 π
16
I
c
2+ h
πB
4
π
I
Section Moment of inertia and section modulus Radius of gyration
+B^2 h h^3
h=H –
πB^3
16
πBh^2
2
+ 2b(h – d)
d^2
4
d^4 +b(h^3 – d^3 )+b^3 (h – d) I
= l
6 h
I
c
=^2 I
H + t
3 π
16
d^4 +b(h^3 + d^3 )+b^3 (h – d)
t
b 2
h
(^2) h^1
H
B
Corrugated sheet iron,
parabolically curved
t
b 1
3 I
t(2B + 5.2H)
r =
I =
=
h 1 =
(b 1 h 13 – b 2 h 23 ), where
(H+t)
h 2 = (H–t)
64
105
2 I
H+t
I
c
1
2
1
2
1
4
1
4
b 1 = (B + 2.6t)
b 2 = (B– 2.6t)