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PROBLEMS (10.1 through 10.4) A cantilever beam is loaded as shown in Figs. P10.1 through
10.4. Using the double-integration method, determine:
(a) The equation of the elastic curve.
(b) The slope at the free end.
(c) The deflection at the free end.
SOLUTION (10.1)
1
(a) EIv " = − wx 2
2
1
EIv ' = − wx 3 + C1
6
1
EIv = − wx 4 + C1 x + C2
24
Boundary conditions:
1
v '( L) = 0 : C1 = wL3
6
1
1
v( L) = 0 : − wL4 + wL4 + C2 ,
24
6
Thus,
w
v' = −
( x3 − L3 )
6 EI
w
v=−
( x 4 − 4 L3 x + 3L4 )
24 EI
(b) x=0 in Eq. (1): θ A =
y
w
A
V
x
1
M = − wx 2
2
1
C2 = − wL4
8
(1)
(2)
wL3
6 EI
(c) x=0 in Eq. (2): v A = −
wL4 wL4
=
↓
8EI 8 EI
SOLUTION (10.2)
M = − P( L − x) = P( x − L)
(a)
y
C
A
2EI
PL
L/2
P
EI
L/2
x
B
P
Segment AC
2 EIv1 '' = P( x − L)
Continued on next slide
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instructional purposes only to students enrolled in courses for which the textbook has been adopted. Any other
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1
P( x − L) 2 + C1
2
1
2 EIv1 = P( x − L)3 + C1 x + C2
6
2 EIv1 ' =
Segment CB
EIv2 '' = P( x − L)
1
EIv2 ' = P( x − L) 2 + C3
2
1
EIv2 = P( x − L)3 + C3 x + C4
6
Boundary conditions:
1
1
v1 '(0) = 0 : C1 = − PL2 ,
v1 (0) = 0 : C2 = PL3
2
6
Thus
P
v1 ' =
( x 2 − 2 xL)
4 EI
P
v1 =
( x 3 − 3 x 2 L)
12 EI
(1)
(2)
Boundary conditions:
L
L
3
1
5
v1 '( ) = v2 '( ) : − PL2 = PL2 + C3 , C3 = − PL2
2
2
16
8
16
L
L
5
1
5
1
v1 ( ) = v2 ( ) : − PL3 = − PL3 − PL3 + C4 , C4 = − PL3
2
2
96
48
32
8
So,
P
5
[( x − L) 2 − L2 ]
2 EI
8
P 1
5
L3
v2 =
[ ( x − L)3 − L2 x + ]
2 EI 3
8
4
v2 ' =
(3)
(4)
(b) x=L in Eq. (3):
θB = −
5 PL2 5 PL2
=
16 EI 16 EI
(c) x=L in Eq. (4):
3 PL3 3 PL3
θB = −
=
↓
16 EI 16 EI
Continued on next slide
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instructional purposes only to students enrolled in courses for which the textbook has been adopted. Any other
reproduction or translation of this work beyond that permitted by Sections 107 or 108 of the 1976 United States
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SOLUTION (10.3)
(a)
x2
w0
2L
1
EIv " = −
w0 x 3
6L
1
EIv ' = −
w0 x 4 + C1
24 L
1
EIv = −
w0 x 5 + C1 x + C2
120 L
y
x
w0
L
A
M =−
x/3
x
Boundary conditions:
1
v '( L) = 0 : C1 =
w0 L3
24
1
1
v( L) = 0 : −
w0 L5 + w0 L4 + C2 = 0
120
24
Therefore
w0
v' =
( x 4 − L4 )
24 EIL
w0
v=−
( x 5 − 5L4 x + 4 L5 )
120 EIL
x3
w0
6L
V
C2 =
1
w0 L3
24
(1)
(2)
(b) x=0 in Eq. (1):
w L2
θA = 0
24 EI
(c) x=0 in Eq. (2):
vA = −
w0 L4 w0 L4
=
↓
30 EI 30 EI
SOLUTION (10.4)
y
(a)
MA =
3 2
wa
2
w
A
a
C
a
B
x
RA= wa
Segment AC
Continued on next slide
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instructional purposes only to students enrolled in courses for which the textbook has been adopted. Any other
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3
wa
(2 x − 3a )
M 1 = − wa 2 + wax =
2
2
wa
EIv1 '' =
(2 x − 3a)
2
wa 2
EIv1 ' =
( x − 3ax) + C1
2
wa x 3 3 2
EIv1 =
( − ax ) + C1 x + C2
2 3 2
Boundary conditions:
v1 '(0) = 0 : C1 = 0,
Thus
wax
v1 ' =
( x − 3a)
2 EI
wax 2
v1 =
(2 x − 9a)
12 EI
(0 ≤ x ≤ a )
v1 (0) = 0 : C2 = 0
(1)
(2)
Segment BC
w
w
M 2 = − (2a − x) 2 = (− x 2 + 4ax − 4a 2 )
2
2
w
EIv2 '' = (− x 2 + 4ax − 4a 2 )
2
w x3
EIv2 ' = (− + 2ax 2 − 4a 2 x) + C3
2
3
w x4 2
EIv2 = (− + ax3 − 2a 2 x 2 ) + C3 x + C4
2 12 3
Continuity conditions:
7
1
v1 '(a) = v2 '(a) : − wa 3 = − wa 3 + C3 ,
C3 = wa 3
6
6
7
13
1
v1 (a) = v2 (a) : − wa 4 = − wa 4 + C4 ,
C4 = − wa 4
12
24
24
Thus
w
(−2 x3 + 12ax 2 − 24a 2 x − 2a 3 )
12 EI
w
v2 =
(− x 4 + 8ax3 − 24a 2 x 2 + 4a 3 x − a 4 )
24 EI
v2 ' =
(3)
(4)
Continued on next slide
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instructional purposes only to students enrolled in courses for which the textbook has been adopted. Any other
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(b) x=2a in Eq. (3):
7 wa 3 7 wa 3
θB = −
=
6 EI
6 EI
(c) x=2a in Eq. (4):
41 wa 4 41 wa 4
vB = −
=
↓
21 EI 21 EI
________________________________________________________________________
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