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sm10 48 51

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PROBLEMS (10.48 through *10.51) A simple beam loaded as shown in Figs. P10.48 through
P10.51. Determine:
(a) The equation of the elastic curve.
(b) The angle of rotation at the end A.
(c) The deflection at the midspan.
SOLUTION (10.48)
(a)
w
y
A
L/2
wL/8
C
L/2
B
x
3wL/8
1
w
L
EIv '' = wLx − < x − > 2
8
2
2
1
w
L
EIv ' = wLx 2 − < x − >3 +C1
16
6
2
1
w
L
EIv =
wLx3 −
< x − > 4 +C1 x + C2
48
24
2
Using boundary conditions:
v(0) = 0 : C2 = 0
(a)
(b)
1
wL4
7
wLx 4 −
+ C1 L = 0,
C1 = −
wL3
48
384
384
Equations (a) and (b) become
w
L
v' =
[24 Lx 2 − 64 < x − >3 −7 L3 ]
384 EI
2
w
L
v=
[8Lx 3 − 16 < x − > 4 −7 L3 x]
384 EI
2
(b) Make x=0 in Eq.(1):
7 wL3
θA =
384 EI
v( L) = 0 :
(1)
(2)
(c) Make x=L/2 in Eq.(2):
5 wL4
vC =
↓
768 EI
Continued on next slide
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SOLUTION (10.49)
(a)
y
M0
A
a
C
b
L
M0/L
x
B
M0/L
M0
x − M 0 < x − a >0
L
M
EIv ' = 0 x 2 + M 0 < x − a > +C1
2L
M0 3 M0
EIv =
x +
< x − a > 2 +C1 x + C2
6L
2
Boundary conditions:
EIv '' =
v(0) = 0 : C2 = 0
(a)
(b)
v( L) = 0 : C1 = −
M0
(3b 2 − L2 )
6L
Equations (a) and (b) become
M0
v' =
[−3x 2 − 6 L < x − a > −(3b 2 − L2 )]
6 EIL
M0
v=
[− x3 + 3L < x − a > 2 −(3b 2 − L2 ) x]
6 EIL
(b) Make x=0 in Eq.(1):
M0
θA =
( L2 − 3b 2 )
6 EIL
(1)
(2)
(c) Make x=L/2 in Eq.(2):
M 0 9 L3
3
vM =
− 3aL2 + 3La 2 − b 2 L)
(
6 EIL 8
2
SOLUTION (10.50)
(a)
y
P
A
a
k
P/2
C
a
B
x
P/2
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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Copyright Act without the permission of the copyright owner is unlawful.
P
x−P < x−a >
2
P
P
EIv ' = x 2 − < x − a > 2 +C1
4
2
P 3 P
EIv = x − < x − a >3 +C1 x + C2
12
6
EIv '' =
(a)
(b)
Boundary conditions:
P
PEI
v(0) = − : C2 = −
2k
2k
3
8Pa Pa 3
PEI
v(2a) = 0 :
−
+ 2C1a −
,
12
6
2k
C1 = −
Pa 2 PEI
+
4
4ak
Equations (a) and (b) become
P
EI
v' =
[ x 2 − 2 < x − a >2 −a 2 + ]
4 EI
ak
P
EI
6 EI
v=
[ x 3 − 2 < x − a >3 +3(− a 2 + ) x −
]
12 EI
ak
k
(1)
(2)
(b) Make x=0 in Eq.(1):
P
EI
θA =
(−a 2 + )
4 EI
ak
(c) Make x=a in Eq.(2):
P
3EI
vC =
(2a 3 +
)↓
12 EI
k
SOLUTION (*10.51)
(a)
2
x
wo
x
w0
L
2w0
y
B
A
L/2
C
L/2
w0L/4
B
w0L/4
(a) Actual load
=
A
C
x
w0L/4
w0L/4 4 w0 ( x − L )
2
L
2w0
(b) Equivalent load
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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Refer to Fig.(b):
wL
x 1 4w
L
L
1 2 x2
1
M = 0 x− (
w0 ) + [ 0 < x − > 2 ] < x − >3
4
2 L
3 2 L
2
3
2
Thus,
wL
w
2w
L
EIv '' = 0 x − 0 x 3 + 0 < x − >3
4
3L
3L
2
w0 L 2 w0 4 w0
L
EIv ' =
x −
x +
< x − > 4 +C1
8
12 L
6L
2
wL
w
w
L
EIv = 0 x 3 − 0 x 5 + 0 < x − >5 +C1 x + C2
24
60 L
30 L
2
(a)
(b)
Boundary conditions:
v(0) = 0 : C2 = 0
v( L) = 0 : C1 = −
5
w0 L3
192
Equations (a) and (b) become
w0
L
v' =
[24 L2 x 2 − 16 x 4 + 32 < x − > 4 −5 L2 ]
192 EIL
2
w0
L
v=
[8L2 x 3 − 3.2 x 5 + 6.4 < x − > 4 −5 L3 x]
192 EIL
2
(1)
(2)
(b) Substitute x=0 into Eq.(1):
5 w0 L2
θA =
192 EI
(c) Substitute x=L/2 into Eq.(2):
w0 L4
vC = vmax =
↓
120 EI
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or
instructional purposes only to students enrolled in courses for which the textbook has been adopted. Any other
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