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Answers to supplementary problems part 2: Δ Wa δ 2.16 in upward δ δ

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Answers to supplementary

problems part 2
Chapter 1
The degree of indeterminacy of the frames are:
S1.1

D1

S1.2

D1

S1.3

D  12

S1.4

D  22

S1.5

(i) D  7
(ii) D  7

S1.6

(i)
(ii)
(iii)
(iv)

D3
D0
D0
D0

S1.7

(i)
(ii)
(iii)
(iv)
(v)

D5
D9
D3
D1
D1

Chapter 2
S2.1

 wa4(4l/3a 1/3)/8EI

S2.2

 2.16 in upward

S2.3

2  0.114 in
3  0.068 in
W  16.75 kips

S2.4

H/V  0.65

S2.5

4  0.59 in

Structural Analysis: In Theory and Practice

600

S2.6

M12  138 kip-in


M21  102 kip-in
M23  112 kip-in
M32  128 kip-in
Q12  Q21  Q23  Q32  2 kips
3  907,200/EI  480/AG

S2.7

M1  20tEI/al2
V1  20tEI/al3
M1  80tEI/a2l4

Chapter 3
S3.1

P24  32.66 kips compression

S3.2

P24  1.07 kips tension


P26  10.33 kips compression

S3.3

P13  W/(5.407  0.472a2A/I) compression

S3.4

P34  11 kips compression

S3.5

P12  132 kips tension

S3.6

H  62.5 kips

S3.7

H  8.28 kips

S3.8

H  0.166W

S3.9

T  20.5 kips

Chapter 4
S4.1

M1  Wab2/l2

S4.2

1  5Wl2/128EI
3  3Wl3/256EI

S4.3

2  wa3(l  a/4)/6EI

S4.4

M12  0.345M
M21  0.147M

S4.5

M12  47.5 kip-ft


M21  31.3 kip-ft

Answers to supplementary problems part 2

S4.6

M12  25.74 kip-ft


M21  32.45 kip-ft

S4.7

M12  101 kip-ft


M21  113 kip-ft

S4.8

M12  Pab(a  b)/l2


M21  Pab(a  b)/l2

S4.9

M12  Pb(l2  b2)/2l2

S4.10

M12  21.45 kip-ft


M21  7.10 kip-ft

601

Chapter 5
S5.1
x/l
V2

S5.2

0.2
0.36

0.4
0.64

0.6
0.84

0.8
0.96

1.0
1.00

For member 12
x/l
M2/l

0.2
0.048

0.4
0.084

0.6
0.096

0.8
0.072

0.2
0.064

0.4
0.072

0.6
0.048

0.8
0.016

For member 23
x/l
M2/l

S5.3
x
H1

0
0.153

20
0.264

40
0.375

60
0.462

80
0.486

5
0.069

6
0.055

S5.4
Panel point
R1

1
1.000

Chapter 6
S6.1

M12  0.345M
M21  0.147M

2
0.610

3
0.264

4
0.000

7
0.000

Structural Analysis: In Theory and Practice

602

S6.2

M12  47.6 kip-ft


M21  31.3 kip-ft

S6.3

M12  2.54 kip-ft

S6.4

M12  25.7 kip-ft


M21  32.5 kip-ft

S6.5

M12  101 kip-ft


M21  133 kip-ft

S6.6

M12  Pab2/l2
M21  Pba2/l2

S6.7

M12  Pb(l2  b2)/2l2

S6.8

s12  0.275EI
c12  0.444
M12  21.55 kip-ft
M21  7.05 kip-ft

S6.9

H  1.08 kips

S6.10

M  34.4 kip-in

S6.11

M12  44 lb-ft


M21  36 lb-ft

Chapter 7
S7.1

V2  7.60 kips
V3  8.32 kips
V4  2.08 kips

S7.2

M1  19 kip-in
V1  2.68 kips
H1  0.48 kips acting to the right
M4  38 kip-in
V4  3.32 kips
H4  1.9 kips acting to the left

S7.3

M2  1682 kip-in
M3  421 kip-in

Answers to supplementary problems part 2

S7.4

M2  3.5 kip-in
M1  10.5 kip-in
M3  0.7 kip-in

S7.5

M2  75 kip-ft
M3  50 kip-ft

S7.6

M2  9.1 kip-ft
M3  13.5 kip-ft
M4  15.1 kip-ft

S7.7

M2  197 kip-in
M3  237 kip-in

S7.8

M12  138 kip-in


M21  102 kip-in
M23  112 kip-in
M32  128 kip-in
M36  128 kip-in
M25  214 kip-in
P12  5.70 kips tension
P23  2.13 kips tension
P36  2.00 kips compression
P25  0 kips
Q12  2.00 kips
Q23  2.00 kips
Q36  2.13 kips
Q25  3.57 kips

S7.9

M12  687 kip-ft


M21  811 kip-ft
M23  347 kip-ft
M32  154 kip-ft
M34  257 kip-ft
M43  242 kip-ft
M45  239 kip-ft
M54  259 kip-ft

S7.10

M12  322 kip-ft


M21  277 kip-ft
M23  184 kip-ft
M32  415 kip-ft
M34  652 kip-ft
M43  548 kip-ft

603

Structural Analysis: In Theory and Practice

604

S7.11

M21  225 kip-ft


M23  28 kip-ft
M32  80 kip-ft
M34  14 kip-ft
M43  22 kip-ft

Chapter 8
S8.1

M30  1351.7  712.8  2064.5 kip-in


V30  94.7  40.5  135.2 kips

S8.2

M1  153 kip-in

S8.3

kW  190

S8.4

P47  8.6 kips

S8.5

(i) lm  lp/120  0.133(EbIb/AtEt)1/3


(ii) M6  250y12/(5)  50y34/(5)  150y5
(iii) The inuence line ordinates for M6 are:
x,ft
I L ordinates for M6

0
40.5

50
21.0

100
0

150
21.0

Chapter 9
S9.1

l/a  3.17
w  58.5Mp/l2

S9.2

S  14.8 in3

S9.3

W/H  8/3 for the beam mode


W/H
2/3 for the sway mode
2/3 W/H 8/3 for the combined mode

S9.4

Mp  9.42 kip-ft for the columns


Mp  18.84 kip-ft for the beams

S9.5

Mp  25 kip-ft for the posts


Mp  50 kip-ft for the chords

S9.6

Mp  Wl
x2  5Mpl2(5)0.5/24EI

200
41.8

250
65.2

Answers to supplementary problems part 2

S9.7

(i) W  2.0Mp/a
(ii) W  3Mp/a
(iii) W  2.80Mp/a

S9.8

Mp  Wa/2

605

Chapter 10
S10.1

The stiffness matrix is:


P 2
20
 EI/l

P 3
6

28

2


3

The final moments are:


M12
M21
M34
M43
S10.2

 42.75 kip-in
 85.5 kip-in
 236.6 kip-in
 181.7 kiip-in

The stiffness matrix is:


P 2
8
 EI/l

P1
2

2 2


4 1

The final moments are:


M21  12 /7 kip-ft
M32  12 /14 kip-ft
S10.3

The stiffness matrix is:


P 2
8

P 3
2

 EI/l

P 4
0

lP
x 2
6
x2  0.136l 2 /EI
4  0.477l/EI
M4  0.285lH

symmetric

6

6

24 x2 /l

Structural Analysis: In Theory and Practice

606

S10.4

The stiffness matrix is:


Px1

 EA/l 2.723

Py1
0.548

0.548 x1


2.296 y1

The member forces are:


P12
P13
P14
P15
S10.5

 0.490W
 0.460W
 1.428W
 0.433W

The stiffness matrix is:


Pxo
3 / 16

Pyo  EA/l 1 / 4

Po
9 / 8

symmetric
3
1/ 2

xo


yo


41 / 4 o

The member forces are:


P1  0.00 kips
P2  8.52 kips
P3  11.48 kips
S10.6

The exibility matrix is:


1
3002

2
0

0 R


3002 R

The cable force is:


R  20.5 kips
S10.7
Then:

The horizontal thrust H may be taken as the redundant.


H  11 kips

Chapter 11
S11.1

Wc  2.55PE

S11.2

Wc  3.1PE

Answers to supplementary problems part 2

S11.3

607

The stiffness matrix is given by


(4  q )
P 2
21
 EI/l

P 3
2

2


(6  q34 ) 3
2

wc  1.55PE /l
S11.4

The stiffness matrix is given by


(2q  q23  q24  q )
2
P 2
r23
r24
25
21



3
P 3  EI/l
r23
(q34  q23 )
r34

r24
r34
(q24  q34  q45 ) 4
P 4
c21  1.055
Load Factor  2.81

S11.5

The stiffness matrix is given by


P 2
(9  4n)
 EI/l

P 3
2  o
Wc  0.455PE

2  o 2


(9  2n) 3

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