30 CHAPTER 1. PROPERTIES OF MATTER
A
B’
B
W
C
D
P Q
O
dy
y
x
dx
dθ
dθ
R
R
l-x
l
Figure 1.25:Neutral surface of a bent cantilever
Hence,
1
R
=
1
(l≠x)
dy
dx
(1.29)
The internal bending moment at point P of the neutral filament is given by the expression
(1.28):
bending moment of the beam =
YIg
R
=
YIg
(l≠x)
dy
dx
(1.30)
whereY is the Young’s Modulus of the material of the cantilever and the geometric
moment of inertiaIg=(bd^3 )/ 12 (for a beam of rectangular cross-section).
Moment of the weightWabout the point P =W(l≠x) (1.31)
At equilibrium, since the moment of the external bending couple (equation1.31) is bal-
anced by the internal bending moment (equation1.30),
W(l≠x)=
YIg
(l≠x)
dy
dx
Rearranging,
dy=
W
YIg
(l≠x)^2 dx (1.32)
The total depressionyat the end of the cantilever is obtained by integrating the expression
(1.32) for the entire length (from 0 tol) of the cantilever.
y=
⁄
dy 0 y=
⁄l
0
W
YIg
(l≠x)^2 dx=
W
YIg
⁄l
0
(l^2 +x^2 ≠ 2 lx)dx=
W
YIg
C
l^2 x+
x^3
3
≠lx^2
Dl
0
Hence,
y=
Wl^3
3 YIg
(1.33)
IfW=mgandIg=(bd^3 )/ 12 ,
y=
(mg)l^3
3 Y
(^1) (bd (^3) )
12
(^2) =
4 Mgl^3
bd^3 Y