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sm10 30 33

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PROBLEM (*10.30 through 10.33) A beam supported and loaded as shown in Figs. P10.30
through P10.33, using a direct-integration method, determine:
(a) The equation of the elastic curve.
(b) The deflection at midspan.
(c) The magnitude and location of the maximum deflection.
(d) The slope at the right end.
SOLUTION (*10.30)
(a)
wo
y
A
RA
xm
RB
B
x
L
x
x2
EIv '''' = − w0
EIv ''' = −
w0 + C1
2L
L
x3
EIv '' = −
w0 + C1 x + C2
6L
1
x4
EIv ' = −
w0 + C1 x 2 + C2 x + C3
24 L
2
5
x
1
1
EIv = −
w0 + C1 x3 + C2 x 2 + C3 x + C4
120 L
6
2
Boundary conditions:
v ''(0) = 0 : C2 = 0
wL
v ''( L) = 0 : C1 = 0
6
v(0) = 0 : C4 = 0
7 w0 L3
v( L) = 0 : C3 = −
360
Equations (1) and (2) become
w0
(−15 x 4 + 30 L2 x 2 − 7 L4 )
v' =
360 EIL
w0 x
(−3 x 4 + 10 L2 x 2 − 7 L4 )
v=
360 EIL
(1)
(2)
(3)
(4)
(b) Make x=L/2 in Eq.(4):
5 w0 L4
vC =
↓
768 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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Set v ' = 0 in Eq.(3):
( c)
8
= 0.5193L
15
xm = L 1 −
Then Eq.(2) gives
vmax
w0 L4
= v( xmax ) = 0.00652
↓
EI
(d) Make x=L in Eq.(1):
w L3
θB = 0
45 EI
SOLUTION (10.31)
(a)
y
L/2
A
xm
M0/L
M0
C
L/2
B
x
M0/L
Due to asymmetric but equal deflection configuration, only segment AC need be
considered.
M0
x
L
M
EIv ' = 0 x 2 + C1
2L
M0 3 1
EIv =
x + C1 x + C2
6L
2
EIv '' =
Boundary conditions:
v(0) = 0 : C2 = 0
M L
L
v( ) = 0 : C1 = − 0
2
12
Then,
M0
(12 x 2 − L2 )
v' =
12 EIL
M0x
(4 x 2 − L2 )
v=
12 EIL
(1)
(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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(b)
Let x=L/2 in Eq.(2):
vC = 0 as required
(c) Set v ' = 0 in Eq.(1):
L
xm =
= 0.2887 L
12
Then, Eq.(2) gives
M 0 L2
M L2
vmax = v( xmax ) = −
= 0.00802 0 ↓
EI
36 12 EI
or, in segment BC:
M L2
vmax = 0.00802 0 ↑
( xm = 0.7113L )
EI
(d) Make x=0 in Eq.(1):
M L2
θ A = −θ B = 0
24 EI
SOLUTION (10.32)
(a)
y
M0
M =−
A
x
V
M0
x + M0
L
RA=M0/L
M0
x + M0
L
M
EIv ' = − 0 x 2 + M 0 x + C1
2L
M0 3 1
EIv = −
x + M 0 x 2 + C1 x + C2
6L
2
EIv '' = −
(a)
(b)
Boundary conditions:
v(0) = 0 : C2 = 0,
1
v( L) = 0 : C1 = M 0 L
3
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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Then Eqs.(a) and Eqs.(b) become
M0
(3 x 2 − 6 Lx + 2 L2 )
v' = −
6 EIL
M x
v = − 0 ( x 2 − 3Lx + 2 L2 )
6 EIL
(1)
(2)
(b) Let x=L/2 in Eq.(b):
M 0 L2
vM =
↓
16 EI
(c) For v ' = 0 , Eq.(1) yields
3x 2 − 6 Lx + 2 L2 = 0 or
Substitute this into Eq.(2):
vmax = v( xm ) = 0.0642
xm = 0.4227 L .
M 0 L2
↓
EI
(d) Making x=L in Eq.(1):
M L
θB = 0
6 EI
SOLUTION (10.33)
y
(a)
w
MA=wL2/8
A
L/2
C
L/2
B
x
RA=wL/2
Segment AC
1
1
1
wLx − wL2 − wx 2
2
8
2
4
w
EIv1 ' = (2 Lx 2 − L2 x − x3 ) + C1
8
3
3
2 2
w 2 Lx L x
x4
EIv1 = (
−
− ) + C1 x + C2
8 3
2
3
EIv1 '' = M 1 =
Segment BC
EIv2 '' = 0
EIv1 ' = C3
EIv = C3 x + C4
(a)
(b)
(c)
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 and continuity condition:
v1 (0) = 0 : C2 = 0
v1 '(0) = 0 : C1 = 0
L
L
wL3
v1 '( ) = v2 '( ) : C3 = −
2
2
48
L
L
wL4
v1 ( ) = v2 ( ) : C4 = −
2
2
384
Then Eqs.(b) and (c) become
wx 2
(4 Lx − 3L2 − 2 x 2 )
v1 =
48 EI
wx3
v2 ' = −
48 EI
wx 3
(−8 x + L)
v2 =
384 EI
(1)
(2)
(3)
(b) Let x=L/2 in Eq.(3)
3 wL4
vC =
↓
384 EI
(c) Let x=L in Eq.(3)
7 wL4
vB =
↓
384 EI
(d) We have
θ B = θC =
wL3
48 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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