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PROBLEMS (10.40 through 10.43) A beam is supported and loaded as shown in Figs. P10.40
through P10.43. Determine:
(a) The equation of the elastic curve.
(b) The slope at the free end.
(c) The deflection at the free end.
SOLUTION (10.40)
(a)
y
3
M A = wa 2
2
w
A
a
C
a
B
x
RA=wa
3
1
EIv '' = wax − wa 2 − w < x − a > 2
2
2
1
3
1
EIv ' = wax 2 − wa 2 x − w < x − a >3 +C1
2
2
6
1
3
1
EIv = wax3 − wa 2 x 2 − w < x − a > 4 +C1 x + C2
6
4
24
Boundary conditions:
v(0) = 0 : C2 = 0
v ' (0) = 0 : C1 = 0
Equation (a) and (b) become
1
wax
EIv ' = − w < x − a >3 −
(3a − x)
6
2
1
wax 2
EIv = − w < x − a > 4 −
(9a − 2 x)
24
12
(a)
(b)
(1)
(2)
(b) Make x=2a in Eq.(1):
7 wa 3
θB =
6 EI
(c) Make x=2a in Eq.(2):
41 wa 4
vB =
↓
24 EI
Continued on next slide
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SOLUTION (10.41)
(a)
y
P
PL
A
L/2
C
L/2
B
x
L
>
2
P
L
EIv ' = PLx − < x − > 2 +C1
2
2
1
P
L
EIv = PLx 2 − < x − >3 +C1 x + C2
2
6
2
EIv '' = PL − P < x −
(a)
(b)
Boundary conditions:
PL2
7
v '( L) = 0 : PL2 −
+ C1 ,
C1 = − PL2
8
8
2
3
3
PL PL 7 PL
19
v( L) = 0 :
−
−
+ C2 = 0,
C2 = − PL3
2
48
8
48
Equations (a) and (b) become
P
L
v' =
[8Lx − 4 P < x − > 2 −7 L2 ]
8 EI
2
P
L
v=
[24 Lx 2 − 8P < x − >3 −42 L2 + 19 L3 ]
48 EI
2
(1)
(2)
(b) Make x=2a in Eq.(1):
7 PL2
θA =
8 EI
(c) Make x=0 in Eq.(2):
19 PL3
vB =
↑
48 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
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SOLUTION (10.42)
(a)
y
w
B
MA=2wa2
A
C
2a
x
a
RA=2wa
1
1
EIv '' = 2 wax − 2 wa 2 − wx 2 + w < x − 2a > 2
2
2
1
1
EIv ' = wax 2 − 2wa 2 x − wx 3 + w < x − 2a >3 +C1
6
6
1
1
1
EIv = wax 3 − wa 2 x 2 − wx 4 + w < x − 2a > 4 +C1 x + C2
3
24
24
Boundary conditions:
v '(0) = 0 : C1 = 0
v(0) = 0 : C2 = 0
Then, Eqs. (a) and (b) become
w
v' =
[6ax 2 − 12a 2 x − x 3 + < x − 2a >3 ]
6 EI
w
v=
[8ax 3 − 24a 2 x 2 − x 4 + < x − 2a > 4 ]
24 EI
(a)
(b)
(1)
(2)
(b) Make x=3a in Eq.(1):
4 wa 3
θB =
3 EI
(c) Make x=3a in Eq.(2):
10 wa 4
vB =
↓
3 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 (10.43)
y
w
A
L
RA
RB
x
C
B
w
M0
Refer to the Fig. P10.43:
1
∑ M A = 0 : − M 0 − 2 wL2 + RB L = 0
M
1
RB = wL + 0
or
L
2
M
1
wL M
∑ Fy = 0 : RA = wL − 2 wL − L0 = 2 − L0
Thus
d 2v
1
1
EI 2 = M ( x) = RA x − wx 2 + RB < x − L > + w < x − L > 2
dx
2
2
dv 1
1
1
1
EI
= RA x 2 − wx3 + RB < x − L > 2 + w < x − L >3 +C1
dx 2
6
2
6
1
1
1
1
EIv = RA x 3 − wx 4 + RB < x − L >3 + w < x − L > 4 +C1 x + C2
6
24
6
24
Boundary conditions:
EIv(0) = 0 : C2 = 0
1
1
EIv( L) = 0 :
RA L3 − wL4 + C1 L = 0
6
24
or
R L2 wL3
wL3 M 0 L
C1 = − A +
=−
+
6
24
24
6
(1)
(2)
Continued on next slide
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Equation (1) and (2) become then
dv
1 wL 2 M 0 2 wx 3 wL M 0
(a)
=θ =
x −
x −
+(
+
[
) < x − L >2
dx
L
L
2 EI 2
3
2
w
wL3 M 0 L
]
+ < x − L >3 −
+
3
12
3
1 wL 3 M 0 x 3 wx 4
wL M 0
v=
[
x −
−
+(
+
) < x − L >3
6 EI 2
L
4
2
L
w
wL3
+ < x − L >4 −
x + M 0 Lx]
4
4
(b)
3L
1 wL3
θC = θ ( ) =
− 5M 0 L)
(
2
6 EI 4
(c) vC = v(
3L
1 9wL4 31
)=
(
− M 0 L2 )
2
24 EI 16
3
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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