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Chapter 16
16.1
1 2 2 3
00
21
0
1 4 1
01 4 1
0012
16.3
[K] =
0
11
1 2 1
011
([K] –
2
2
3
21 41
11 612
x
AE AL
x
L
=
2 =
22
60 60 36
7 7 7
4 (1)
2
=
1 = 0.649
2 = 7.922
16.4 (a) Two equal length elements
From Problem 16.3 results
[M] =
00
21
0
1 4 1
601 4 1
0012
AL
2 [M]) {X} = 0
or
0
1 4 1
0
2
1 1 1 4 1
260
1 1 2
01
= 0
= 0
16.5
t0 = 0 d0 = d0dot = 0
d–1 = 0 – 0 +
25 = 0.01125 ft
= 0.01125 ft
d2 =
{(0.03)2 (66.67) + (2 2 – 0.032 2000 0.01125}
1
2
1
2
ft
t3 = 0.09 s
0.06 0.039319 1.084121 2.347196 83.33333 602.8986
0.12 0.081832 –0.13384 –44.3317 75 1254.753
0.18 0.011632 –1.62917 13.3684 50 178.3512
16.6
(a) Using central difference
d0 = 0, d0dot = 0
t = 0.02 s
[K] = k = 1200
d0dotdot =
[20 – 1200 (0)] = 10
{d–1} = 0 – (0.02) (0) +
(10) = 0.002 ft
= 0.002 ft
= 0.00672 ft
d3 = 0.01223 ft
d2dotdot =
(12 – 1200 (0.00672)) = 1.968
d2dot =
= 0.2558
Step 3 t = 0.06 s F3 = 8 lb
= 0.0164 ft
Step 4 t = 0.08 s F4 = 4 lb
= 0.01743 ft
d4dot =
= 0.13
Step 5 t = 0.10 s F5 = 0
= 0.01428 ft
Summary
(b) Newmark’s time integration method (Mathcad solution)
F0 = 20 lb K = 1200
M = 2 slug M = 2
t = 0.02s
d2 =
d2 = 6.252 10–3 ft
Acceleration at t = 0.04
F1prime = F1 +
[6d0 + 6(t)d0dot + 2(t)2d0dotdot]
F1prime = 56 lb
d1 =
d1 = 1.795 10–3 ft
Acceleration at t = 0.02
d1dotdot =
(d1 – d0) –
d0dot – 2 d0dotdot d1dotdot = 6.923
Velocity at t = 0.02
d1dot =
(d1 – d0) – 2 d0dot –
d0dotdot d1dot = 0.169
d2 =
d2 = 6.252 10–3 ft
Acceleration at t = 0.04
d2dotdot =
(d2 – d1) –
d1dot – 2 d1dotdot d2dotdot = 2.249
F4 =
F0 F4 = 4 lb
F4prime = F4 +
[6 d3 + 6(t)d3dot + 2(t)2d3dotdot]
= 0.167 K 31200
= 0.5
K31200
16.10
[K] =
= 104
= 25.7
t
=
= 0.058 s
16.11
Global stiffness matrix
v1
v2
2 v3
3
22
12 6 12 6 0 0
6 4 6 2 0 0
12 6 24 0 12 6
LL
L L L L
LL
[m] =
1 0 0 0 0 0
0 0 0 0 0 0
002000
0 0 0 0 0 0
0 0 0 0 1 0
0 0 0 0 0 0