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PROBLEMS (10.44 through 10.47) For the beam loaded and supported as shown in Figs.
P10.44 through P10.47, determine:
(a) The equation of the deflection curve.
(b) The slope at end B for the given numerical values:
P = 4 kips, a = 3 ft, L = 10 ft, E = 10 x 106 psi,
I = 72 in.4 ,
w=2 kips/ft
SOLUTION (10.44)
y
P
B
MA=3Pa
A
x
C a
3a
RA=P
(a)
EIv '' = Px − 3Pa − P < x − 3a >
1
1
EIv ' = Px 2 − 3Pax − P < x − 3a > 2 +C1
2
2
1
3
1
EIv = Px3 − Pax 2 − P < x − 3a >3 +C1 x + C2
6
2
6
Boundary conditions:
v '(0) = 0 : C1 = 0
v(0) = 0 : C2 = 0
Equations (a) and (b) become
P
v' =
[3x 2 − 18ax − 3 < x − 3a > 2 ]
6 EI
P 3
v=
[ x − 9ax 2 − < x − 3a >3 ]
6 EI
(a)
(b)
(1)
(2)
(b) Make x=4a in Eq.(1):
9 Pa 2
θB =
2 EI
9(4 ×103 )(36) 2
=
= 32.4 × 10−3 rad .
2(10 ×106 )(72)
SOLUTION (10.45)
(a)
y
A
P
P
P
C
D
L
B
x
P
Continued on next slide
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EIv '' = Px − P < x − a > − P < x − L + a >
Px 2 P
P
EIv ' =
− < x − a > 2 − < x − L + a > 2 +C1
2
2
2
3
Px P
P
EIv =
− < x − a >3 − < x − L + a > 3 +C1 x + C2
6
6
6
Boundary conditions:
L
PL2 P L
Pa
v '( ) = 0 :
− ( − a) + C1 = 0,
C1 =
(a − L)
2
8
2 2
2
v(0) = 0 : C2 = 0
Equations (a) and (b) become
P
v' =
[ x 2 − < x − a > 2 − < x − L + a > 2 + a(a − L)]
2 EI
P 3
v=
[ x − < x − a >3 − < x − L + a >3 +3ax(a − L)]
6 EI
(b)
(a)
(b)
(1)
(2)
Make x=L in Eq.(1):
Pa
θB =
( L − a)
2 EI
4 × 103 (3 × 12)(10 − 3)12
=
= 8.4 × 10−3 rad .
2(10 × 106 )(72)
SOLUTION (10.46)
(a)
y
P
Pa
A
RA =
2a
P
4
C
L
2a
B
RB =
x
3P
4
Px
− P < x − 2a > + Pa < x − 2a > 0
4
Px 2 P
EIv ' =
− < x − 2a > 2 + Pa < x − 2a > +C1
8
2
3
Px P
Pa
EIv =
− < x − 2a > 3 +
< x − 2a > 2 +C1 x + C2
24 6
2
EIv '' =
(a)
(b)
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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Boundary conditions:
v(0) = 0 : C2 = 0
v(4a ) = 0 :
64 3 8 3
Pa − Pa + 2 Pa 3 + 4aC1 = 0,
24
6
C1 = −
Equations (a) and (b) become
P
v' =
[3x 2 − 12 < x − 2a > 2 +24a < x − 2a > −20a 2 ]
24 EI
P
v=
[ x3 − 4 < x − 2a >3 +12a < x − 2a > 2 −20a 2 x]
24 EI
5Pa 2
6
(1)
(2)
(b) Make 4a in Eq.(1):
7 Pa 2
θB =
6 EI
7(4 ×103 )(3 ×12) 2
=
= 8.4 ×10−3 rad
6(10 × 106 )(72)
SOLUTION (10.47)
C
A
M(x)
L/2
x
RA
2w
dV
L
= w= − 0 < x− >
2
dx
L
w0
dM
L 2
=V = −
< x − > + RA
2
dx
L
w
L
M ( x ) = − 0 < x − > 3 + RA x
3L
2
At x = L,
M ( L) = 0 : 0 = −
w0
L
( L − ) 3 + RA L
3L
2
or
RA =
w0 L
24
Therefore
w
wL
d 2v
L
EI 2 = M ( x) = − 0 < x − >3 + 0 x
dx
3L
2
24
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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w
wL
dv
L
= − 0 < x − > 4 + 0 x 2 + C1
dx
12 L
2
48
w
wL
L
EIv = − 0 < x − >5 + 0 x 3 + C1 x + C2
60 L
2
144
EI
Boundary conditions:
EIv(0) = 0 : C2 = 0
EIv( L) = 0 : −
(a) v =
(b)
w0 L 5 wL4
( ) +
+ C1 L = 0,
60 L 2
144
C1 = −
37 w0 L3
5760
w0
1
L
L2 3 37 L4
[− < x − >5 +
x −
x]
EIL 60
5
144
5760
dv w0
1
L
L2
37 L4
=
[− < x − > 4 + x 2 −
]
dx EIL 12
5
48
5760
37 w0 L3
θ A = v '(0) =
5760 EI
Substituting the given data
37(2 × 103 )(10 × 12)3
θA =
= 0.03083 rad = 1.77 o
5760(10 × 106 )(72)
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
reproduction or translation of this work beyond that permitted by Sections 107 or 108 of the 1976 United States
Copyright Act without the permission of the copyright owner is unlawful.
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