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Similar to Cap 03 mecanica vectorial para ingenieros estatica 8ed. (20)
Cap 03 mecanica vectorial para ingenieros estatica 8ed.
- 1. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 1.
Resolve 90 N force into vector components P and Q
where Q = (90 N)sin 40°
= 57.851 N
Then MB = −rA/BQ
= −(0.225 m)(57.851 N)
= −13.0165 N⋅m
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
MB = 13.02 N⋅m W
- 2. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 2.
Fx = (90 N)cos 25°
= 81.568 N
Fy = (90 N)sin 25°
= 38.036 N
x = (0.225 m)cos65°
= 0.095089 m
y = (0.225 m)sin 65°
= 0.20392 m
MB = xFy − yFx
= (0.095089 m)(38.036 N) − (0.20392 m)(81.568 N)
= −13.0165 N⋅m
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
MB = 13.02 N⋅m W
- 3. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 3.
Px = (3 lb)sin 30°
= 1.5 lb
Py = (3 lb)cos30°
= 2.5981 lb
MA = xB/A Py + yB/A Px
= (3.4 in.)(2.5981 lb) + (4.8 in.)(1.5 lb)
= 16.0335 lb⋅in.
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
MA = 16.03 lb⋅in. W
- 4. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 4.
For P to be a minimum, it must be perpendicular to the line joining points
A and B
with ( )2 ( )2 rAB = 3.4 in. + 4.8 in.
= 5.8822 in.
tan 1 y
α = θ = −
x
−
tan 1 4.8 in.
=
3.4 in.
= 54.689°
Then MA = rAB Pmin
P M
or min
19.5 lb in.
5.8822 in.
A
AB
r
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
⋅
= =
= 3.3151 lb
∴Pmin = 3.32 lb 54.7°
or Pmin = 3.32 lb 35.3° W
- 5. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 5.
By definition MA = rB/A Psinθ
where θ = φ + (90° −α )
φ −
=
and tan 1 4.8 in.
3.4 in.
= 54.689°
Also ( )2 ( )2
rB/A = 3.4 in. + 4.8 in.
= 5.8822 in.
Then (17 lb⋅in.) = (5.8822 in.)(2.9 lb)sin (54.689° + 90° −α )
or sin (144.689° −α ) = 0.99658
or 144.689° −α = 85.260°; 94.740°
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
∴α = 49.9°, 59.4° W
- 6. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 6.
(a)
(b)
(a) MA = rB/A × TBF
MA xTBFy yTBFx = +
= (2 m)(200 N)sin 60° + (0.4 m)(200 N)cos60°
= 386.41 N⋅m
φ −
= = °
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or MA = 386 N⋅m W
(b) For FC to be a minimum, it must be perpendicular to the line
joining A and C.
( )∴MA = d FC min
with ( )2 ( )2 d = 2 m + 1.35 m
= 2.4130 m
Then ( )( )min 386.41 N⋅m = 2.4130 m FC
( )min FC = 160.137 N
and tan 1 1.35 m 34.019
2 m
θ = 90 − φ = 90° − 34.019° = 55.981°
( )min ∴ FC = 160.1 N 56.0° W
- 7. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 7.
(a)
(b)
(c)
MA = xTBF + yTBF
y x
= (2 m)(200 N)sin 60° + (0.4 m)(200 N)cos60°
= 386.41 N⋅m
M = xF
= = ⋅
= 193.205 N
⋅ = F
F =
θ −
= = °
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
AM = ⋅
or 386 N m
Have A C
or
386.41 N m
2 m
A
C
M
F
x
∴F = 193.2 N
C For B
F to be minimum, it must be perpendicular to the line joining A
and B
( )A B min
∴M = d F
with ( ) ( ) 2 2
d = 2 m + 0.40 m = 2.0396 m
Then 386.41 N m ( 2.0396 m
)( )C
min
( )min
189.454 N
C
and 1 2 m
tan 78.690
0.4 m
or ( )min
F = 189.5 N
78.7°
C
- 8. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 8.
(a)
(b)
(c)
( ) /
M = r cos15
° W
B AB
= (14 in.)(cos15°)(5 lb)
= 67.615 lb⋅in.
M = r P °
M = r F
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
BM = ⋅
or 67.6 lb in.
/
sin85
B DB
67.615 lb⋅in. = (3.2 in.)Psin85°
or P = 21.2 lb
For ( )min,
F F must be perpendicular to BC.
Then, B C/B
67.615 lb⋅in. = (18 in.)F
or F = 3.76 lb 75.0°
- 9. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 9.
(a) Slope of line
EC= =
T = T
ABx AB
= =
T = =
M = T − T
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
35 in. 5
+
76 in. 8 in. 12
Then ( ) 12
13
( ) 12
260 lb 240 lb
13
and ( ) 5
260 lb 100 lb
13 ABy
Then (35 in.) (8 in.)
D ABx ABy
= (240 lb)(35 in.) − (100 lb)(8 in.)
= 7600 lb⋅in.
DM = ⋅
or 7600 lb in.
(b) Have ( ) ( ) D ABx ABy M = T y + T x
= (240 lb)(0) + (100 lb)(76 in.)
= 7600 lb⋅in.
DM = ⋅
or 7600 lb in.
- 10. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 10.
Slope of line
35 in. 7
EC= =
+
112 in. 8 in. 24
Then
24
T = T
ABx AB
25
and
7
T = T
ABy AB
25
Have ( ) ( ) D ABx ABy M = T y + T x
( ) ( ) 24 7
∴ ⋅ = T + T
7840 lb in. 0 112 in.
AB AB
25 25
250 lb
T =
AB
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
T =
or 250 lb
AB
- 11. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 11.
The minimum value of d can be found based on the equation relating the moment of the force TAB about D:
( ) ( ) max D ABy
M = T d
where MD = 1152 N⋅m
( ) ( ) ABmax y ABmax sin 2880 N sin T = T θ = θ
Now
sin 1.05 m
( )2 ( )2
d 0.24 1.05 m
θ =
+ +
1152 N m 2880 N 1.05
∴ ⋅ =
( ) 2 2
( 0.24 ) ( 1.05
)
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
d
d
+ +
or ( )2 ( )2 d + 0.24 + 1.05 = 2.625d
or (d + 0.24)2 + (1.05)2 = 6.8906d 2
or 5.8906d 2 − 0.48d − 1.1601 = 0
Using the quadratic equation, the minimum values of d are 0.48639 m and −0.40490 m.
Since only the positive value applies here, d = 0.48639 m
or d = 486 mm W
- 12. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 12.
with ( )2 ( )2 dAB = 42 mm + 144 mm
= 150 mm
sin 42 mm
150 mm
θ =
cos 144 mm
150 mm
θ =
and FAB = − FAB sinθ i − FAB cosθ j
2.5 kN ( 42 mm) (144 mm)
150 mm
= − i − j
= −(700 N)i − (2400 N) j
Also ( ) ( ) rB/C = − 0.042 m i + 0.056 m j
Now MC = rB/C × FAB
= (−0.042i + 0.056 j) × (−700i − 2400 j)N⋅m
= (140.0 N⋅m)k
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or MC = 140.0 N⋅m W
- 13. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 13.
with ( )2 ( )2 dAB = 42 mm + 144 mm
= 150 mm
sin 42 mm
150 mm
θ =
cos 144 mm
150 mm
θ =
FAB = − FAB sinθ i − FAB cosθ j
2.5 kN ( 42 mm) (144 mm)
150 mm
= − i − j
= −(700 N)i − (2400 N) j
Also ( ) ( ) rB/C = − 0.042 m i − 0.056 m j
Now MC = rB/C × FAB
= (−0.042i − 0.056j) × (−700i − 2400j)N⋅m
= (61.6 N⋅m)k
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or MC = 61.6 N⋅m W
- 14. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 14.
: (0.090 m) 88 80 N (0.280 m) 105 80 N
D D 137 137 ΣM M = × − ×
= −12.5431 N⋅m
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or MD = 12.54 N⋅m W
- 15. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 15.
Note: B = B(cosβ i + sinβ j)
B′ = B(cosβ i − sinβ j)
C = C(cosαi + sinα j)
By definition: B × C = BCsin (α − β ) (1)
B′ × C = BCsin (α + β ) (2)
Now ... B × C = B(cosβ i + sinβ j) × C(cosα i + sinα j)
= BC(cosβ sinα − sinβ cosα )k (3)
and B′ × C = B(cosβ i − sinβ j) × C(cosαi + sinα j)
= BC(cosβ sinα + sinβ cosα )k (4)
Equating the magnitudes of B × C from equations (1) and (3) yields:
BCsin (α − β ) = BC(cosβ sinα − sinβ cosα ) (5)
Similarly, equating the magnitudes of B′ × C from equations (2) and (4) yields:
BCsin (α + β ) = BC(cosβ sinα + sinβ cosα ) (6)
Adding equations (5) and (6) gives:
sin (α − β ) + sin (α + β ) = 2cosβ sinα
or sin cos 1 sin ( ) 1 sin ( )
α β = α + β + α − β W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
2 2
- 16. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 16.
Have d = λAB × rO/A
r
B A
where /
rB A
/
AB
=
λ
and rB/A = (−210 mm − 630 mm)i
+ (270 mm − (−225 mm))j
= −(840 mm)i + (495 mm) j
( )2 ( )2
rB/A = −840 mm + 495 mm
= 975 mm
−
(840 mm) + (495 mm)
Then =
i j
AB 975 mm λ
1 ( 56 33 )
65
= − i + j
Also rO/A = (0 − 630)i + (0 − (−225)) j
= −(630 mm)i + (225 mm) j
1 ( 56 33 ) (630 mm) (225 mm)
65
∴ d = − i + j × − i + j
= 126.0 mm
d = 126.0 mm W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 17. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 17.
(a)
= ×
A B
×
A B
λ
where A = 12i − 6j + 9k
B = −3i + 9j − 7.5k
Then
i j k
× = −
12 6 9
− −
3 9 7.5
A B
= (45 − 81)i + (−27 + 90) j + (108 − 18)k
= 9(−4i + 7j + 10k)
And 2 2 2 A × B = 9 (−4) +(7) +(10) = 9 165
9( − 4 + 7 +
10 )
∴ = i j k λ
9 165
or ( ) 1
A B
i j k
× = − −
−
− + −
∴ = i j k λ
λ = − i + j − k
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
λ = − 4 i + 7 j + 10
k
165
(b)
= ×
×
A B
λ
where A = −14i − 2j + 8k
B = 3i + 1.5j − k
Then
14 2 8
3 1.5 1
A B
= (2 − 12)i + (24 − 14) j + (−21 + 6)k
= 5(−2i + 2j − 3k)
and 2 2 2 A × B = 5 (−2) + (2) + (−3) = 5 17
5( 2 2 3 )
5 17
1
or ( 2 2 3
) 17
- 18. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 18.
(a) Have A = P × Q
i j k
3 7 2 in.2
5 1 3
P Q
× = −
−
= [(21 + 2)i + (10 − 9)j + (3 + 35)k]in.2
= (23 in.2 )i + (1 in.2 )j + (38 in.2 )k
∴ A = (23)2 + (1)2 + (38)2 = 44.430 in.2
i j k
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or A = 44.4 in.2 W
(b) A = P × Q
2 4 3 in.2
6 1 5
× = −
−
P Q
= [(−20 − 3)i + (−18 − 10)j + (−2 + 24)k] in.2
= −(23 in.2 )i − (28 in.2 )j + (22 in.2 )k
∴ A = (−23)2 + (−28)2 + (22)2 = 42.391 in.2
or A = 42.4 in.2 W
- 19. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 19.
(a) Have MO = r × F
i j k
6 3 1.5 N m
7.5 3 4.5
= − ⋅
−
= [(−13.5 − 4.5)i + (11.25 − 27)j + (−18 − 22.5)k] N⋅m
= (−18.00i − 15.75j − 40.5k) N⋅m
or MO = −(18.00 N⋅m)i − (15.75 Ν⋅m)j − (40.5N⋅m)k W
(b) Have MO = r × F
i j k
2 0.75 1 Nm
7.5 3 4.5
= − − ⋅
−
= [(3.375 + 3)i + (−7.5 + 9)j + (6 + 5.625)k] N⋅m
= (6.375i + 1.500j + 11.625k) N⋅m
or MO = (6.38 N⋅m)i + (1.500 Ν⋅m)j + (11.63 Ν⋅m)k W
(c) Have MO = r × F
i j k
= − − ⋅
2.5 1 1.5 N m
7.5 3 4.5
= [(4.5 − 4.5)i + (11.25 − 11.25)j + (−7.5 + 7.5)k] N⋅m
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or MO = 0 W
This answer is expected since r and F are proportional (F = −3r). Therefore, vector F has a line of action
passing through the origin at O.
- 20. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 20.
(a) Have MO = r × F
i j k
= − − ⋅
7.5 3 6 lb ft
3 −
6 4
= [(12 − 36)i + (−18 + 30)j + (45 − 9)k] lb⋅ft
or MO = −(24.0 lb⋅ft)i + (12.00 lb⋅ft) j + (36.0 lb⋅ft)k W
(b) Have MO = r × F
i j k
= − − ⋅
7.5 1.5 1 lb ft
3 −
6 4
= [(6 − 6)i + (−3 + 3)j + (4.5 − 4.5)k] lb⋅ft
or MO = 0 W
(c) Have MO = r × F
i j k
= − − ⋅
8 2 14 lb ft
3 −
6 4
= [(8 − 84)i + (−42 + 32)j + (48 − 6)k] lb⋅ft
or MO = −(76.0 lb⋅ft)i − (10.00 lb⋅ft) j + (42.0 lb⋅ft)k W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 21. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 21.
With TAB = −(369 N) j
( ) ( ) ( ) ( )
i − j −
k
2.4 m 3.1 m 1.2 m
( )2 ( )2 ( )2
369 N
+ − + −
2.4 m 3.1 m 1.2 m
JJJG
T AD
= =
T
AB AD
AD
TAD = (216 N)i − (279 N) j − (108 N)k
Then RA = 2 TAB + TAD
= (216 N)i − (1017 N) j − (108 N)k
Also ( ) ( ) rA/C = 3.1 m i + 1.2 m k
Have MC = rA/C × RA
i j k
= ⋅
0 3.1 1.2 Nm
216 − 1017 −
108
= (885.6 N⋅m)i + (259.2 N⋅m) j − (669.6 N⋅m)k
MC = (886 N⋅m)i + (259 N⋅m) j − (670 N⋅m)k W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 22. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 22.
Have MA = rC/A × F
where ( ) ( ) ( ) rC/A = 215 mm i − 50 mm j + 140 mm k
Fx = −(36 N)cos 45°sin12°
Fy = −(36 N)sin 45°
Fz = −(36 N)cos 45°cos12°
∴ F = −(5.2926 N)i − (25.456 N) j − (24.900 N)k
i j k
A = − ⋅
M
and 0.215 0.050 0.140 N m
− − −
5.2926 25.456 24.900
= (4.8088 N⋅m)i + (4.6125 N⋅m) j − (5.7377 N⋅m)k
MA = (4.81 N⋅m)i + (4.61 N⋅m) j − (5.74 N⋅m)k W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 23. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 23.
Have MO = rA/O × R
where ( ) ( ) rA/D = 30 ft j + 3 ft k
( ) ( ) T1 = − 62 lb cos10° i − 62 lb sin10° j
= −(61.058 lb)i − (10.766 lb) j
JJJG
T AB
AB
T =
2 2
( ) ( ) ( ) ( )
i − j +
k
5 ft 30 ft 6 ft
( )2 ( )2 ( )2
62 lb
+ − +
5 ft 30 ft 6 ft
=
= (10 lb)i − (60 lb) j + (12 lb)k
∴ R = −(51.058 lb)i − (70.766 lb) j + (12 lb)k
i j k
O = ⋅
0 30 3lbft
51.058 70.766 12
− −
M
= (572.30 lb⋅ft)i − (153.17 lb⋅ft) j + (1531.74 lb⋅ft)k
MO = (572 lb⋅ft)i − (153.2 lb⋅ft) j + (1532 lb⋅ft)k W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 24. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 24.
(a) Have MO = rB/O × TBD
where rB/O = (2.5 m)i + (2 m) j
JJJG
T BD
T =
BD BD
BD
( ) ( ) ( ) ( )
− 1 m i − 2 m j + 2 m
k
=
( )2 ( )2 ( )2
900 N
1m 2 m 2 m
− + − +
= −(300 N)i − (600 N) j + (600 N)k
Then
i j k
O= ⋅
2.5 2 0 N m
300 600 600
− −
M
MO = (1200 N⋅m)i − (1500 N⋅m) j − (900 N⋅m)k W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
continued
- 25. COSMOS: Complete Online Solutions Manual Organization System
(b) Have MO = rB/O × TBE
where rB/O = (2.5 m)i + (2 m) j
JJJG
T BE
T =
BE BE
BE
( ) ( ) ( ) ( )
− 0.5 m i − 2 m j − 4 m
k
=
( )2 ( )2 ( )2
675 N
0.5 m + − 2 m + −
4 m
= −(75 N)i − (300 N) j − (600 N)k
Then
i j k
O= ⋅
2.5 2 0 N m
75 300 600
− − −
M
MO = −(1200 N⋅m)i + (1500 N⋅m) j − (600 N⋅m)k W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 26. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 25.
Have MC = rA/C × P
where
rA/C = rB/C + rA/B
= (16 in.)(−cos80°cos15°i − sin80°j − cos80°sin15°k)
+(15.2 in.)(−sin 20°cos15°i + cos 20°j − sin 20°sin15°k)
= −(7.7053 in.)i − (1.47360 in.) j − (2.0646 in.)k
and P = (150 lb)(cos5°cos70°i + sin 5°j − cos5°sin 70°k)
= (51.108 lb)i + (13.0734 lb) j − (140.418 lb)k
Then
i j k
C = − − − ⋅
7.7053 1.47360 2.0646 lb in.
51.108 13.0734 −
140.418
M
= (233.91 lb⋅in.)i − (1187.48 lb⋅in.) j − (25.422 lb⋅in.)k
or MC = (19.49 lb⋅ft)i − (99.0 lb⋅ft) j − (2.12 lb⋅ft)k W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 27. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 26.
Have MC = rA/C × FBA
where ( ) ( ) ( ) rA/C = 0.96 m i − 0.12 m j + 0.72 m k
and FBA = λBAFBA
− ( 0.1 m ) i + ( 1.8 m ) j − ( 0.6 m
)
k
=
( ) + ( ) + ( )
( ) 2 2 2
i j k
∴ C = − ⋅
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
228 N
0.1 1.8 0.6 m
= −(12.0 N)i + (216 N) j − (72 N)k
0.96 0.12 0.72 N m
12.0 216 72
− −
M
= −(146.88 N⋅m)i + (60.480 N⋅m) j + (205.92 N⋅m)k
or MC = −(146.9 N⋅m)i + (60.5 N⋅m) j + (206 N⋅m)k W
- 28. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 27.
Have MC = TAD d
where d = Perpendicular distance from C to line AD
T AD
i j k
2.4 m 3.1 m 1.2 m
i j k
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
JJJG
with MC = rA/C TAD
and ( ) ( ) rA/C = 3.1 m j + 1.2 m k
AD AD
AD
T =
JJJG
( ) ( ) ( ) ( )
( )2 ( )2 ( )2
369 N
2.4 m 3.1 m 1.2 m
AD
− − =
+ − + −
T
= (216 N)i − (279 N) j − (108 N)k
Then
0 3.1 1.2 Nm
216 279 108
C= ⋅
− −
M
= (259.2 N⋅m) j − (669.6 N⋅m)k
and ( )2 ( )2 MC = 259.2 N⋅m + −669.6 N⋅m
= 718.02 N⋅m
∴ 718.02 N⋅m = (369 N)d
or d = 1.946 m W
- 29. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 28.
M = T
Have O AC d
where d = Perpendicular distance from O to rope AC
with MO = rA/O × TAC
and ( ) ( ) rA/O = 30 ft j + 3 ft k
TAC = − (62 lb)cos10° i − (62 lb)sin10° j
= −(61.058 lb)i − (10.766 lb) j
Then
i j k
0 30 3lbft
61.058 10.766 0
O= ⋅
− −
M
= (32.298 lb⋅ft)i − (183.174 lb⋅ft) j + (1831.74 lb⋅ft)k
and ( )2 ( )2 ( )2 MO = 32.298 lb⋅ft + −183.174 lb⋅ft + 1831.74 lb⋅ft
= 1841.16 lb⋅ft
∴1841.16 lb⋅ft = (62 lb)d
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or d = 29.7 ft W
- 30. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 29.
Have MO = TAB d
where d = Perpendicular distance from O to rope AB
with MO = rA/O × TAB
and ( ) ( ) rA/O = 30 ft j + 3 ft k
JJJG
T AB
T =
AB AB
AB
( ) ( ) ( ) ( )
5 ft i − 30 ft j + 6 ft
k
=
( )2 ( )2 ( )2
62 lb
5 ft + − 30 ft +
6 ft
= (10 lb)i − (60 lb) j + (12 lb)k
Then
i j k
0 30 3 lbft
10 60 12
O = ⋅
−
M
= (540 lb⋅ft)i + (30 lb⋅ft) j − (300 lb⋅ft)k
and ( )2 ( )2 ( )2 MO = 540 lb⋅ft + 30 lb⋅ft + −300 lb⋅ft
= 618.47 lb⋅ft
∴ 618.47 lb⋅ft = (62 lb)d
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or d = 9.98 ft W
- 31. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 30.
Have MC = TBD d
where d = Perpendicular distance from C to cable BD
with MC = rB/C × TB/D
and ( ) rB/C = 2 m j
JJJG
T BD
T =
BD BD
BD
( ) ( ) ( ) ( )
− 1m i − 2 m j + 2 m
k
=
( )2 ( )2 ( )2
900 N
1m 2 m 2 m
− + − +
= −(300 N)i − (600 N) j + (600 N)k
Then
i j k
0 2 0 Nm
300 600 600
C= ⋅
− −
M
= (1200 N⋅m)i + (600 N⋅m)k
and ( )2 ( )2 MC = 1200 N⋅m + 600 N⋅m
= 1341.64 N⋅m
∴1341.64 = (900 N)d
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or d = 1.491 m W
- 32. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 31.
Have MC = Pd
From the solution of problem 3.25
MC = (233.91 lb⋅in.)i − (1187.48 lb⋅in.) j − (25.422 lb⋅in.)k
Then
( ) ( ) ( ) 2 2 2 MC = 233.91 + −1187.48 + −25.422
= 1210.57 lb⋅in.
d MC
and 1210.57 lb.in.
150 lb
= =
P
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or d = 8.07 in.W
- 33. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 32.
Have |MD | = FBAd
where d = perpendicular distance from D to line AB.
MD = rA/D × FBA
( ) ( ) rA/D = − 0.12 m j + 0.72 m k
( ( 0.1m ) i ( 1.8 m ) j ( 0.6 m
) k
)
( ) 2 2 2
( ) ( ) ( )
i j k
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
228 N
0.1 1.8 0.6 m
BA BAFBA
− + −
= =
+ +
F λ
= −(12.0 N)i + (216 N) j − (72 N)k
0 0.12 0.72 N m
12.0 216 72
∴ D = − ⋅
− −
M
= −(146.88 N⋅m)i − (8.64 N⋅m) j − (1.44 N⋅m)k
and ( )2 ( )2 ( )2 |MD | = 146.88 + 8.64 + 1.44 = 147.141N⋅m
∴ 147.141N⋅m = (228 N)d
d = 0.64536 m
or d = 0.645 mW
- 34. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 33.
Have |MC | = FBAd
where d = perpendicular distance from C to line AB.
MC = rA/C × FBA
( ) ( ) ( ) rA/C = 0.96 m i − 0.12 m j + 0.72 m k
( ( 0.1m ) i ( 1.8 m ) j ( 0.6
) k
)
( ) ( ) ( )
( ) 2 2 2
i j k
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
228 N
0.1 1.8 0.6 m
BA BAFBA
− + −
= =
+ +
F λ
= −(12.0 N)i + (216 N) j − (72 N)k
0.96 0.12 0.72 N m
12.0 216 72
∴ C = − ⋅
− −
M
= −(146.88 N⋅m)i − (60.48 N⋅m) j + (205.92 N⋅m)k
and ( )2 ( )2 ( )2 |MC | = 146.88 + 60.48 + 205.92 = 260.07 N⋅m
∴ 260.07 N⋅m = (228 N)d
d = 1.14064 m
or d = 1.141mW
- 35. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 34.
(a) Have d = rC/A sinθ = λAB × rC/A
where d = Perpendicular distance from C to pipe AB
with
λ AB i j k
7 + 4 −
32
7 4 32
( )2 ( )2 ( )2
= =
AB AB
+ + −
1 (7 4 32 )
33
= i + j − k
and ( ) ( ) ( ) rC/A = − 14 ft i + 5 ft j + L − 22 ftk
λ r
Then /
i j k
1 7 4 32 ft
33
× = −
L
14 5 22
AB C A
− −
1 { 4( 22) 32(5) 32(14) 7( 22) 7(5) 4(14) }ft
33
= L − + i + − L − j + + k
= 1 (4 L + 72) i + ( − 7 L + 602) j + 91 kft
33
and d = 1 (4 L + 72)2 + ( − 7 L + 602)2 +
(91)2
33
2
d dd L L
( ) , 1 2 4 4 72 2 7 7 602 0
For ( )( ) ( )( )
= + + − − + =
min 2
L
d 33
or 65L − 3926 = 0
or L = 60.400 ft
But L Lgreenhouse so L = 30.0 ft W
(b) with L = 30 ft, d = 1 (4 × 30 + 72)2 + ( − 7 × 30 + 602)2 +
(91)2
33
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or d = 13.51 ft W
Note: with L = 60.4 ft,
1 (4 60.4 72)2 ( 7 60.4 602)2 (91)2 11.29 ft
33
d= × + + − × + + =
- 36. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 35.
P⋅Q = (−4i + 8j − 3k) ⋅ (9i − j − 7k)
= (−4)(9) + (8)(−1) + (−3)(−7)
= −23
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or P⋅Q = −23W
P⋅S = (−4i + 8j − 3k) ⋅ (5i − 6j + 2k)
= (−4)(5) + (8)(−6) + (−3)(2)
= −74
or P⋅S = −74 W
Q⋅S = (9i − j − 7k) ⋅ (5i − 6j + 2k)
= (9)(5) + (−1)(−6) + (−7)(2)
= 37
or Q⋅S = 37 W
- 37. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 36.
By definition
B⋅C = BCcos(α − β )
where B = B (cosβ )i + (sinβ ) j
C = C (cosα )i + (sinα ) j
∴ (Bcosβ )(C cosα ) + (Bsinβ )(Csinα ) = BC cos(α − β )
or cosβ cosα + sinβ sinα = cos(α − β ) (1)
By definition
B′⋅C = BC cos(α + β )
where B′ = (cosβ )i − (sinβ ) j
∴ (Bcosβ )(Ccosα ) + (−Bsinβ )(Csinα ) = BCcos(α + β )
or cosβ cosα − sinβ sinα = cos(α + β ) (2)
Adding Equations (1) and (2),
2 cosβ cosα = cos(α − β ) + cos(α + β )
or cos cos 1 cos( ) 1 cos( )
α β = α + β + α − β W
2 2
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 38. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 37.
First note:
rB/A = (0.56 m)i + (0.9 m) j
( ) ( ) rC/A = 0.9 m j − 0.48 m k
( ) ( ) ( ) rD/A = − 0.52 m i + 0.9 m j + 0.36 m k
( )2 ( )2
rB/A = 0.56 m + 0.9 m = 1.06 m
( )2 ( )2
rC/A = 0.9 m + −0.48 m = 1.02 m
( )2 ( )2 ( )2
rD/A = −0.52 m + 0.9 m + 0.36 m = 1.10 m
By definition rB/A ⋅rD/A = rB/A rD/A cosθ
or (0.56i + 0.9j) ⋅ (−0.52i + 0.9j + 0.36k) = (1.06)(1.10)cosθ
(0.56)(−0.52) + (0.9)(0.9) + (0)(0.36) = 1.166cosθ
cosθ = 0.44494
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
θ = 63.6° W
- 39. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 38.
From the solution to problem 3.37
rC/A = 1.02 m with rC/A = (0.9 m)i − (0.48 m) j
( ) ( ) ( ) rD/A = 1.10 m with rD/A = − 0.52 m i + 0.9 m j + 0.36 m k
Now by definition
rC/A ⋅ rD/A = rC/A rD/A cosθ
or (0.9j − 0.48k) ⋅ (−0.52i + 0.9j + 0.36k) = (1.02)(1.10)cosθ
0(−0.52) + (0.9)(0.9) + (−0.48)(0.36) = 1.122cosθ
cosθ = 0.56791
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or θ = 55.4° W
- 40. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 39.
(a) By definition
λBC + λEF = (1)(1) cosθ
where
( ) ( ) ( )
( )2 ( )2 ( )2
i j k
32 ft 9 ft 24 ft
32 9 24 ft
BC
− −
=
+ − + −
λ
1 (32 9 24 )
41
= i − j − k
( ) ( ) ( )
( )2 ( )2 ( )2
i j k
14 ft 12 ft 12 ft
14 12 12 ft
EF
− − +
=
− + − +
λ
1 ( 7 6 6 )
11
= − i − j + k
(32 i − 9 j − 24 k ) ( − 7 i − 6 j +
6 k
)
Therefore ⋅ =
cos
41 11
θ
(32)(−7) + (−9)(−6) + (−24)(6) = (41)(11)cosθ
cosθ = −0.69623
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or θ = 134.1° W
(b) By definition ( EG )BC ( EF )cos T = T θ
= (110 lb)(−0.69623)
= −76.585 lb
or ( EF )BC 76.6 lb T = − W
- 41. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 40.
(a) By definition
λBC ⋅ λEG = (1) (1) cosθ
where
( ) ( ) ( )
( )2 ( )2 ( )2
i j k
32 ft 9 ft 24 ft
32 9 24 ft
BC
− −
=
+ − + −
λ
1 (32 9 24 )
41
= i − j − k
( ) ( ) ( )
i j k
16 ft − 12 ft +
9.75
16 12 9.75 ft
( )2 ( )2 ( )2
EG
=
+ − +
λ
1 (16 12 9.75 )
22.25
= i − j + k
(32 i − 9 j − 24 k ) (16 i − 12 j +
9.75 k
)
Therefore ⋅ =
cos
41 22.25
θ
(32)(16) + (−9)(−12) + (−24)(9.75) = (41)(22.25)cosθ
cosθ = 0.42313
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or θ = 65.0° W
(b) By definition ( EG )BC ( EG )cos T = T θ
= (178 lb)(0.42313)
= 75.317 lb
or ( EG )BC 75.3 lb T = W
- 42. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 41.
First locate point B:
3.5
d =
22 14
or d = 5.5 m
(a) ( )2 ( )2 ( )2 dBA = 5.5 + 0.5 + −22 + −3 = 23 m
Locate point D:
(−3.5 − 7.5sin 45°cos15°), (14 + 7.5cos 45°),
(0 + 7.5sin 45°sin15°)m
or (−8.6226 m, 19.3033 m, 1.37260 m)
Then
( )2 ( )2 ( )2 dBD = −8.6226 + 5.5 + 19.3033 − 22 + 1.37260 − 0 m
= 4.3482 m
⋅ ( 6 i − 22 j − 3 k ) ⋅ ( − 3.1226 i − 2.6967 j +
1.37260
k
)
and ( )( )
cos
23 4.3482
d d
d d
BA BD
θ
ABD
= =
BA BD
= 0.36471
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or θ ABD = 68.6° W
(b) ( BA )BD BA cos ABD T = T θ
= (230 N)(0.36471)
or ( BA )BD 83.9 N T = W
- 43. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 42.
First locate point B:
3.5
d =
22 14
or d = 5.5 m
(a) Locate point D:
(−3.5 − 7.5sin 45°cos10°), (14 + 7.5cos 45°),
3.2227 2.6967 0.92091 5.2227 5.3033 0.92091
d d
d d
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
(0 + 7.5sin 45°sin10°)m
or (−8.7227 m, 19.3033 m, 0.92091 m)
Then
dDC = (5.2227 m)i − (5.3033 m) j − (0.92091 m)k
and
( )2 ( )2 ( )2 dDB = −5.5 + 8.7227 + 22 − 19.3033 + 0 − 0.92091 m
= 4.3019 m
and ( ) ( )
( )( )
cos
4.3019 7.5
DB DC
BDC
DB DC
θ
⋅ + − ⋅ − −
= =
i j k i j k
= 0.104694
or θ BDC = 84.0° W
(b) ( BD )DC BD cos BDC (250 N)(0.104694) T = T θ =
or ( BD )DC 26.2 N T = W
- 44. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 43.
Volume of parallelopiped is found using the mixed triple product
(a) Vol = P⋅(Q × S)
3 4 1
7 6 8 in.
9 2 3
3
−
= − −
− −
= (−54 + 288 + 14 − 48 + 84 − 54)in.3
= 230 in.3
5 7 4
6 2 5 in.
4 8 9
− −
= −
− −
= (−90 + 140 + 192 + 200 − 378 − 32) in.3
= 32 in.3
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or Volume = 230 in.3 W
(b) Vol = P⋅(Q × S)
3
or Volume = 32 in.3 W
- 45. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 44.
For the vectors to all be in the same plane, the mixed triple product is zero.
P⋅(Q × S) = 0
3 7 5
− −
0 2 1 4
∴ = − −
8 Sy −
6
0 = 18 + 224 − 10Sy − 12Sy + 84 − 40
So that 22 Sy = 286
Sy = 13
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or Sy = 13.00 W
- 46. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 45.
Have rC = (2.25 m)k
JJJG
T CE
T =
CE CE
CE
( ) ( ) ( ) ( )
0.90 m i + 1.50 m j − 2.25 m
k
=
( )2 ( )2 ( )2
1349 N
0.90 1.50 2.25 m
T
CE
+ + −
= (426 N)i + (710 N) j − (1065 N)k
Now MO = rC × TCE
i j k
0 0 2.25 Nm
426 710 1065
= ⋅
−
= − (1597.5 N⋅m)i + (958.5 N⋅m) j
∴ Mx = −1598 N⋅m, My = 959 N⋅m, Mz = 0 W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 47. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 46.
Have rE = (0.90 m)i + (1.50 m) j
JJJG
T DE
T =
DE DE
DE
( ) ( ) ( ) ( )
− 2.30 m i + 1.50 m j − 2.25 m
k
=
( )2 ( )2 ( )2
1349 N
2.30 1.50 2.25 m
− + + −
= −(874 N)i + (570 N) j − (855 N)k
Now MO = rE × TDE
i j k
0.90 1.50 0 N m
874 570 855
= ⋅
− −
= −(1282.5 N⋅m)i + (769.5 N⋅m) j + (1824 N⋅m)k
∴Mx = −1283 N⋅m, My = 770 N⋅m, Mz = 1824 N⋅m W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 48. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 47.
Have z ( B )y BA ( C )y CD
= ⋅ × + × M k r T k r T
where Mz = −(48 lb⋅ft)k
( B )y ( C )y (3 ft) r = r = j
( ) ( ) ( ) ( )
JJJG
4.5 ft i − 3 ft j + 9 ft
k
= =
( )2 ( )2 ( )2
14 lb
4.5 3 9 ft
T BA
T
BA BA
BA
+ − +
= (6 lb)i − (4 lb) j + (12 lb)k
( ) ( ) ( )
( )2 ( )2 ( )2
JJJG
i − j − k
= =
6 ft 3 ft 6 ft
6 3 6 ft
T CD T
T
CD CD CD
CD
+ − + −
= TCD i − j − k
(2 2 )
3
Then −(48 lb⋅ft) = k⋅{(3 ft) j × (6 lb)i − (4 lb) j + (12 lb)k}
+ k ⋅(3 ft) j × TCD (2 i − j − 2 k
)
3
or −48 = −18 − 2TCD
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
TCD = 15.00 lb W
- 49. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 48.
Have y ( B )z BA ( C )z CD
M = j⋅ r × T × j⋅ r × T
where My = 156 lb⋅ft
( B )z (24 ft) ; ( C )z (6 ft) r = k r = k
( ) ( ) ( )
( )2 ( )2 ( )2
JJJG
i − j + k
= =
4.5 ft 3 ft 9 ft
4.5 3 9 ft
T BA T
T
BA BA BA
BA
+ − +
= TBA i − j + k
(4.5 3 9 )
10.5
( ) ( ) ( ) ( )
JJJG
6 ft i − 3 ft j + 9 ft
k
= =
( )2 ( )2 ( )2
7.5 lb
6 3 9 ft
T CD
T
CD CD
CD
+ − +
= (5 lb)i − (2.5 lb) j − (5 lb)k
⋅ = ⋅ × TBA − +
Then (156 lb ft) j (24 ft) k (4.5 i 3 j 9 k
)
10.5
+ j⋅{(6 ft)k × (5 lb)i − (2.5 lb) j − (5 lb)k}
or 156 108 30
10.5 BA = T +
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
TBA = 12.25 lb W
- 50. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 49.
Based on Mx = (Pcosφ )(0.225 m)sinθ − (Psinφ )(0.225 m)cosθ (1)
My = −(Pcosφ )(0.125 m) (2)
Mz = −(Psinφ )(0.125 m) (3)
By ( )
M P
M P
Equation 3 sin 0.125
( )
( )( )
( )( )
:
z
y
φ
φ
−
=
−
Equation 2 cos 0.125
−
or 4 tan 9.8658
23
= ∴ = °
φ φ
−
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or φ = 9.87° W
From Equation (2)
−23 N⋅m = −(Pcos9.8658°)(0.125 m)
P = 186.762 N
or P = 186.8 N W
From Equation (1)
26 N⋅m = (186.726 N)cos9.8658° (0.225 m)sinθ
− (186.726 N)sin 9.8658° (0.225 m)cosθ
or 0.98521sinθ − 0.171341cosθ = 0.61885
Solving numerically,
θ = 48.1° W
- 51. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 50.
Based on Mx = (Pcosφ )(0.225 m)sinθ − (Psinφ )(0.225 m)cosθ (1)
My = −(Pcosφ )(0.125 m) (2)
Mz = −(Psinφ )(0.125 m)
By ( )
M P
M P
Equation 3 sin 0.125
( )
( )( )
( )( )
:
z
y
φ
φ
−
=
−
Equation 2 cos 0.125
or 3.5 tan ; 9.9262
20
φ φ
−
= = °
−
From Equation (3):
−3.5 N⋅m = −(Psin 9.9262°)(0.125 m)
P = 162.432 N
From Equation (1):
Mx = (162.432 N)(0.225 m)(cos9.9262°sin 60° − sin 9.9262°cos60°)
= 28.027 N⋅m
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or Mx = 28.0 N⋅m W
- 52. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 51.
First note:
JJJG
T BA
T =
BA BA
BA
( ) ( ) ( ) ( )
+ − + + − =
i j k
L
L
4 1.5 1 6
BC
( ) ( ) ( ) 2 2 2
70 lb
+ − + + −
4 1.5 1 6
BC
( ) ( )
i L
j k
4 + 0.5 − −
6
BC
( )2
70 lb
52 0.5
L
BC
=
+ −
rA = (4 ft)i + (1.5 ft) j − (12 ft)k
Have MO = rA × TBA
70 lb 4 ft 1.5 ft 12 ft
= −
( ) ( ) 2
52 + 0.5 − L BC 4 0.5 − L
BC −
6 763 lb ft 70 1.5 6 12 0.5 lb ft
− ⋅ = − + − ⋅
2 190.81 190.81 4 25.19 6198.8225
− ± − −
=
BC 2 25.19 L
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
i j k
For the i components:
( )
( ) ( ) 2
52 + 0.5
BC
BC
L
L
−
or ( )2 10.9 52 + 0.5 − LBC = 3 + 12LBC
or (10.9)2 52 + (0.5 − LBC )2 = 9 + 72LBC + 144L2BC
or 25.19L2BC + 190.81LBC − 6198.8225 = 0
Then
( ) ( )( )
( )
Taking the positive root LBC = 12.35 ft W
- 53. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 52.
First note:
JJJG
T BA
T =
BA BA
BA
( ) ( ) ( ) ( )
+ − + + − =
i j k
L
L
4 1.5 1 6
BC
( ) ( ) ( ) 2 2 2
70 lb
+ − + + −
4 1.5 1 6
BC
( ) ( )
i L
j k
4 + 0.5 − −
6
BC
( )2
70 lb
52 0.5
L
BC
=
+ −
rA = (4 ft)i + (1.5 ft) j − (12 ft)k
Have MO = rA × TBA
BA
i j k
= −
( ) ( ) 2
T BA
L
− ⋅ = − + − ⋅
L
T BA
L
= +
L
T BA
L
− ⋅ = − − ⋅
L
T L
315 4 BA
1
= +
L
1 300 1 4
2 315 41 BC
L
L
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
4 ft 1.5 ft 12 ft
52 + 0.5 4 0.5 6
BC BC
T
L L
− − −
For the i components:
( )
( ) ( ) 2
900 lb ft 1.5 6 12 0.5 lb ft
52 + 0.5
BC
BC
−
or
( )
( ) 2
300 1 4
52 + 0.5
BC
BC
−
(1)
For the k components:
( )
( ) ( ) 2
315 lb ft 4 0.5 1.5 4 lb ft
52 + 0.5
BC
BC
−
or
( )
( ) 2
52 + 0.5
BC
BC
−
(2)
Then, ( )
( ) ( )
BC
+
⇒ =
+
or 59 ft
BC 4 L =
LBC = 14.75 ft W
- 54. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 53.
Have MAD = λ AD ⋅(rB/A × TBH )
where ( ) ( )
i k
0.8 m −
0.6 m
λ = = i −
k
( )2 ( )2
0.8 0.6
0.8 m 0.6 m
AD
+ −
( ) rB/A = 0.4 m i
( ) ( ) ( ) ( )
JJJJG
0.3 m i + 0.6 m j − 0.6 m
k
= =
( )2 ( )2 ( )2
1125 N
0.3 0.6 0.6 m
T BH
T
BH BH
BH
+ + −
Then
0.8 0 0.6
0.4 0 0 180 N m
375 750 750
MAD
−
= =− ⋅
−
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or MAD = −180.0 N⋅m W
- 55. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 54.
Have MAD = λ AD ⋅(rB/A × TBG )
where λ AD = (0.8 m)i − (0.6 m)k
( ) rB/A = 0.4 m i
( ) ( ) ( ) ( )
JJJG
− 0.4 m i + 0.74 j − 0.32 m
k
= =
( )2 ( )2 ( )2
1125 N
0.4 m 0.74 m 0.32 m
T BG
T
BG BG
BG
− + + −
= −(500 N)i + (925 N) j − (400 N)k
Then
0.8 0 0.6
0.4 0 0
500 925 400
MAD
−
=
− −
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or MAD = −222 N⋅m W
- 56. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 55.
Have
MAD = λ AD ⋅(rE/A × FEF )
λ =
where AD
JJJG
AD
AD
( 7.2 m ) i ( 0.9 m
)
j
( 7.2 m )2 ( 0.9 m
)2
AD
+
=
+
λ
= 0.99228i + 0.124035 j
( ) ( ) rE/A = 2.1 m i − 0.9 m j
( ) ( ) ( ) ( )
JJJG
0.3 m i + 1.2 m j + 2.4 m
k
= =
( )2 ( )2 ( )2
24.3 kN
0.3 m 1.2 m 2.4 m
F EF
F
EF EF
EF
+ +
= (2.7 kN)i + (10.8 kN) j + (21.6 kN)k
Then
0.99228 0.124035 0
2.1 0.9 0 kN m
2.7 10.8 21.6
MAD = − ⋅
= −19.2899 − 5.6262
= −24.916 kN⋅m
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or MAD = −24.9 kN⋅m W
- 57. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 56.
Have MAD = λ AD ⋅(rG/A × EEF )
Where ( ) ( )
i j
7.2 m +
0.9 m
7.2 m 0.9 m
( )2 ( )2
AD
=
+
λ
= 0.99228i + 0.124035 j
( ) ( ) rG/A = 6 m i − 1.8 m j
( ) ( ) ( ) ( )
JJJJG
− 1.2 m i + 2.4 m j + 2.4 m
k
= =
( )2 ( )2 ( )2
21.3 kN
1.2 m 2.4 m 2.4 m
F GH
F
GH GH
GH
− + +
= −(7.1 kN)i + (14.2 kN) j + (14.2 kN)k
Then
0.99228 0.124035 0
MAD = − ⋅
6 1.8 0 kNm
7.1 14.2 14.2
−
= −25.363 − 10.5678
= −35.931 kN⋅m
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or MAD = −35.9 kN⋅m W
- 58. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 57.
Have M = λ ⋅ ( r × P
)
OA OA C/O where
From triangle OBC
a
( ) 2 x
OA =
( ) ( ) 1
tan30
2 3 2 3 z x
OA = OA + OA + OA
2 2
= a + + a
a OA
∴ OA = a − − = a
OAλ = i + j + k
P = λ P
° − °
P = i − k
∴ =
aP
= − −
aP =
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
a a
OA OA
= ° = =
Since ( ) ( ) ( ) ( ) 2 2 2 2
x y z
or ( )
2 2
2 y 2 3
( )
2 2
a a
2 2
y 4 12 3
Then /
2
2 3 2 3
AO
a a
r = i + a j + k
and
1 2 1
2 3 2 3
BC
( asin30 ) ( acos30
)( P
) a
=
i k
( 3 )
2
C/O r = ai
( )
1 2 1
2 3 2 3
1 0 0 2
1 0 3
OA
P
M a
−
2
( 1 )( 3
) 2 3
2
2
OA
aP
M =
- 59. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 58.
(a) For edge OA to be perpendicular to edge BC,
OA BC = 0 uuur uuur ⋅⋅⋅⋅
where
From triangle OBC
a
( OA ) =
x
2 ( ) ( ) 1
tan30
2 3 2 3 z x
∴ = + +
i j k
OA OA
= a a i − k
= a ( i − 3 k
)
a
i + a a
OA
j + k ⋅⋅⋅⋅ i − k
=
2 2
a a
+ OA − =
M = Pd with P acting along BC and d the
uuur uuur
Pa
∴ = Pd
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
a a
OA OA
= ° = =
a a
( )
2 y 2 3
uuur
uuur
and BC = (asin 30°)i − (acos30°)k
3
2 2
2
Then ( ) ( 3 ) 0
2 y 2 3 2
or ( ) ( )
0 0
4 y 4
∴ OA BC = 0 uuur uuur ⋅⋅⋅⋅
uuur
so that OA
uuur
is perpendicular to . BC
(b) Have OA ,
perpendicular distance from OA to BC.
From the results of Problem 3.57,
2
OA
Pa
M =
2
or
a
d =
2
- 60. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 59.
Have MDI = λDI ⋅(rF/I × TEF )
where ( ) ( )
i j
( )2 ( )2
T EF
3.6 ft i − 10.8 ft j + 16.2 ft
k
=
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
4.8 ft 1.2 ft
4.8 ft 1.2 ft
DI
DI
DI
−
= =
+ −
λ
JJJG
= 0.97014i − 0.24254 j
( ) rF/I = 16.2 ft k
EF EF
EF
T =
JJJG
( ) ( ) ( ) ( )
( )2 ( )2 ( )2
29.7 lb
3.6 ft + − 10.8 ft +
16.2 ft
= (5.4 lb)i − (16.2 lb) j + (24.3 lb)k
Then
0.97014 0.24254 0
0 0 16.2lbft
5.4 16.2 24.3
MDI
−
= ⋅
−
= −21.217 + 254.60
= 233.39 lb⋅ft
or MDI = 233 lb⋅ft W
- 61. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 60.
Have MDI = λDI ⋅(rG/I × TEG )
where ( ) ( )
i j
4.8 ft 1.2 ft
4.8 ft 1.2 ft
( )2 ( )2
DI
DI
DI
T EG
3.6 ft i − 10.8 ft j − 35.1 ft
k
=
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
−
= =
+ −
λ
JJJG
= 0.97014i − 0.24254 j
( ) rG/I = − 35.1 ft k
EG EG
EG
T =
JJJG
( ) ( ) ( ) ( )
( )2 ( )2 ( )2
24.6 lb
3.6 ft + − 10.8 ft + −
35.1 ft
= (2.4 lb)i − (7.2 lb) j − (23.4 lb)k
Then
0.97014 0.24254 0
0 0 35.1lbft
2.4 7.2 23.4
MDI
−
= − ⋅
− −
= 20.432 − 245.17
= −224.74 lb⋅ft
or MDI = −225 lb⋅ft W
- 62. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 61.
First note that F1 = F1λ1 and F2 = F2λ2
Let M1 = moment of F2 about the line of action of M1
and M2 = moment of F1 about the line of action of M2
Now, by definition
( ) ( ) M1 = λ1 ⋅ rB/A × F2 = λ1 ⋅ rB/A × λ2 F2
( ) ( ) M2 = λ2 ⋅ rA/B × F1 = λ2 ⋅ rA/B × λ1 F1
Since F1 = F2 = F and rA/B = −rB/A
( ) M1 = λ1 ⋅ rB/A × λ2 F
( ) M2 = λ2 ⋅ −rB/A × λ1 F
Using Equation (3.39)
( ) ( ) λ1 ⋅ rB/A × λ2 = λ2 ⋅ −rB/A × λ1
so that ( ) M2 = λ1 ⋅ rB/A × λ2 F
∴ M12 = M21W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 63. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 62.
From the solution of Problem 3.53:
λAD = 0.8i − 0.6k
TBH = (375 N)i + (750 N) j − (750 N)k; TBH = 1125 N
MAD = −180 N⋅m
Only the perpendicular component of TBH contributes to the moment of TBH about line AD. The
parallel component of TBH will be used to find the perpendicular component.
Have ( )TBH Parallel = λAD ⋅TBH
= [0.8i − 0.6k] ⋅ (375 N)i + (750 N) j − (750 N)k
= (300 + 450)N
= 750 N
Since ( ) ( ) TBH = TBH Perpendicular + TBH Parallel
Then ( ) ( )2 ( )2
TBH Perpendicular = TBH − TBH Parallel
( )2 ( )2 = 1125 N − 750 N
= 838.53 N
and ( )MAD = TBH Perpendicular d
180 N⋅m = (838.53 N)d
d = 0.21466 m
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or d = 215 mm W
- 64. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 63.
From the solution of Problem 3.54:
λAD = 0.8i − 0.6k
(500 N) (925 N) (400 N)
1125 N
T i j k
BG
TBG
= − + −
=
MAD = −222 N⋅m
Only the perpendicular component of TBG contributes to the moment of TBG about line AD. The
parallel component of TBG will be used to find the perpendicular component.
Have ( )TBG Parallel = λAD ⋅TBG
= [0.8i − 0.6k] ⋅ −(500 N)i + (925 N) j − (400 N)k
= (−400 + 240)N
= −160 N
Since ( ) ( ) TBG = TBG Perpendicular + TBG Parallel
Then ( ) ( )2 ( )2
TBG Perpendicular = TBG − TBG Parallel
( )2 ( )2 = 1125 N − −160 N
= 1113.56 N
and ( )MAD = TBG Perpendicular d
222 N⋅m = (1113.56 N)d
d = 0.199361 m
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or d = 199.4 mm W
- 65. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 64.
From the solution of Problem 3.59:
λDI = 0.97014i − 0.24254 j
(5.4 lb) (16.2 lb) (24.3 lb)
29.7 lb
T i j k
EF
TEF
= − +
=
MDI = 233.39 lb⋅ft
Only the perpendicular component of TEF contributes to the moment of TEF about line DI. The
parallel component of TEF will be used to find the perpendicular component.
Have ( )TEF Parallel = λDI ⋅TEF
= [0.97014i − 0.24254 j] ⋅ (5.4 lb)i − (16.2 lb) j + (24.3 lb)k
= (5.2388 + 3.9291)
= 9.1679 lb
Since ( ) ( ) TEF = TEF Perpendicular + TEF Parallel
Then ( ) ( )2 ( )2
TEF Perpendicular = TEF − TEF Parallel
( )2 ( )2 = 29.7 − 9.1679
= 28.250 lb
and ( )MDI = TEF Perpendicular d
233.39 lb⋅ft = (28.250 lb)d
d = 8.2616 ft
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or d = 8.26 ft W
- 66. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 65.
From the solution of Problem 3.60:
λDI = 0.97014i − 0.24254 j
(2.4 lb) (7.2 lb) (23.4 lb)
24.6 lb
T i j k
EG
TEG
= − −
=
MDI = − 224.74 lb⋅ft
Only the perpendicular component of TEG contributes to the moment of TEG about line DI. The
parallel component of TEG will be used to find the perpendicular component.
Have ( )TEG Parallel = λDI ⋅TEG
= [0.97014 i − 0.24254 j] ⋅ (2.4 lb) i − (7.2 lb) j − (23.4 lb)k
= (2.3283 + 1.74629)
= 4.0746 lb
Since ( ) ( ) TEG = TEG Perpendicular + TEG Parallel
Then ( ) ( )2 ( )2
TEG Perpendicular = TEG − TEG Parallel
( )2 ( )2 = 24.6 − 4.0746
= 24.260 lb
and ( )MDI = TEG Perpendicular d
224.74 lb⋅ft = (24.260 lb)d
d = 9.2638 ft
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or d = 9.26 ft W
- 67. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 66.
From the solution of Prob. 3.55:
λAD = 0.99228i + 0.124035 j
FEF = (2.7 kN)i + (10.8 kN) j + (21.6 kN)k
FEF = 24.3 kN
MAD = −24.916 kN⋅m
Only the perpendicular component of FEF contributes to the moment of FEF about edge AD. The
parallel component of FEF will be used to find the perpendicular component.
Have ( )FEF Parallel = λAD ⋅FEF
= [0.99228i + 0.124035 j] ⋅ (2.7 kN)i + (10.8 kN) j + (21.6 kN)k
= 4.0187 kN
Since ( ) ( ) FEF = FEF Perpendicular + FEF Parallel
Then ( ) ( )2 ( )2
FEF Perpendicular = FEF − FEF Parallel
( )2 ( )2 = 24.3 − 4.0187
= 23.965 kN
and ( )MAD = FEF Perpendicular d
24.916 kN⋅m = (23.965 kN)d
d =1.039683m or d = 1.040 m W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 68. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 67.
From the solution of Prob. 3.56:
λAD = 0.99228i + 0.124035 j
FGH = −(7.1 kN)i + (14.2 kN) j + (14.2 kN)k
FGH = 21.3 kN
MAD = −35.931 kN⋅m
Only the perpendicular component of FGH contributes to the moment of FGH about edge AD. The
parallel component of FGH will be used to find the perpendicular component.
Have ( )FGH Parallel = λAD ⋅FGH
= (0.99228i + 0.124035 j) ⋅ −(7.1 kN)i + (14.2 kN) j + (14.2 kN)k
= −5.2839 kN
Since ( ) ( ) FGH = FGH Perpendicular + FGH Parallel
Then ( ) ( )2 ( )2
FGH Perpendicular = FGH − FGH Parallel
( )2 ( )2 = 21.3 − 5.2839
= 20.634 kN
and ( )MAD = FGH Perpendicular d
35.931 kN⋅m = (20.634 kN)d
d = 1.741349m or d = 1.741 m W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 69. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 68.
(a) Have M1 = d1F1
Where d1 = 0.6 m and F1 = 40 N
( )( ) ∴ M1 = 0.6 m 40 N
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or M1 = 24.0 N⋅m W
(b) Have MTotal = M1 + M2
8 N⋅m = 24.0 N⋅m − (0.820 m)(cosα )(24 N)
∴ cosα = 0.81301
or α = 35.6° W
(c) Have M1 + M2 = 0
( ) 24 N⋅m − d2 24 N = 0
or d2 = 1.000 m W
- 70. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 69.
(a) M = Fd
12 N⋅m = F (0.45 m)
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or F = 26.7 N W
(b) M = Fd
12 N⋅m = F (0.24 m)
or F = 50.0 N W
(c) M = Fd
( )2 ( )2 Where d = 0.45 m + 0.24m
= 0.51 m
12 N⋅m = F (0.51 m)
or F = 23.5 N W
- 71. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 70.
(a) Note when a = 8 in., rC/F is perpendicular to the inclined 10 lb forces.
Have M = ΣFd ( )
= −(10 lb)a + 8 in. + 2(1 in.) − (10 lb)2a 2 + 2(1 in.)
For a = 8 in.,
M = −(10 lb)(18 in. + 24.627 in.)
= −426.27 lb⋅in.
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or M = 426 lb⋅in. W
(b) Have M = 480 lb⋅in.
Also M = Σ(M + Fd ) ( )
= Moment of couple due to horizontal forces at A and D +
Moment of force-couple systems at C and F about C.
Then −480 lb⋅in. = −10 lb a + 8 in. + 2(1 in.) + MC + MF + FX (a + 8 in.) + Fy (2a)
Where MC = −(10 lb)(1 in.) = −10 lb⋅in.
MF = MC = −10 lb⋅in.
Fx −
=
10 lb
2 Fy −
=
10 lb
2 ∴ −480 lb⋅in. = −10 lb(a + 10 in.) − 10 lb⋅in. − 10 lb⋅in.
10 lb ( 8 in.) 10 lb (2 )
2 2
− a + − a
303.43 = 31.213 a
or a = 9.72in.W
- 72. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 71.
(a) Have M = ΣFd ( )
= (9 lb)(13.8 in.) − (2.5 lb)(15.2 in.)
= (86.2 lb⋅in.)
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
M = 86.2 lb⋅in. W
(b) Have M = Td = 86.2 lb⋅in.
For T to be a minimum, d must be maximum.
∴Tmin must be perpendicular to line AC.
tan 15.2 in.
11.4 in.
θ =
θ = 53.130°
or θ = 53.1° W
(c) Have M = Tmindmax Where M = 86.2 lb⋅in.
( )2 ( )2 ( )
dmax = 15.2 in. + 11.4 in. + 2 1.2 in.
= 21.4 in.
( ) ∴86.2 lb⋅ in. = Tmin 21.4 in.
Tmin = 4.0280 lb
or Tmin = 4.03 lb W
- 73. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 72.
Based on M = M1 + M2
( ) M1 = 18 N⋅m k
( ) M2 = 7.5 N⋅m i
∴M = (7.5 N⋅m)i + (18 N⋅m)k
and ( )2 ( )2 M = 7.5 N⋅m + 18 N⋅m
= 19.5 N⋅m
M ⋅ i + ⋅
k λ
= =
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or M = 19.50 N⋅m W
With (7.5 N m) (18 N m)
M 19.5 N ⋅
m
5 12
13 13
= i + k
Then cos 5 67.380
x 13 x θ = ∴θ = °
cosθ y = 0 ∴θ y = 90°
cos 12 22.620
z 13 z θ = ∴θ = °
or θ x = 67.4°, θ y = 90.0°, θ z = 22.6° W
- 74. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 73.
Have M = M1 + M2
Where M1 = rC/B × PIC
( ) ( ) rC/B = 38.4 in. i − 16 in. j
PIC = −(25 lb)k
i j k
M
1 38.4 16 0 lb in.
∴ = − ⋅
0 0 −
25
= (400 lb⋅in.)i + (960 lb⋅in.) j
and M2 = rD/A × PZE
( ) ( ) rD/A = 8 in. j − 22 in. k
( ) ( ) ( )
JJJG
− 19.2 in. i + 22 in.
k
= =
( )2 ( )2
36.5 lb
19.2 in. 22 in.
P ED
P
ZE ZE
ED
− +
= −(24 lb)i + (27.5 lb)k
i j k
2 0 8 22lbin.
M
∴ = − ⋅
24 0 27.5
−
( ) ( ) ( ) M2 = 220 lb⋅in. i + 528 lb⋅in. j + 192 lb⋅in. k
and M = M1 + M2
= (400 lb⋅in.)i + (960 lb⋅in.) j + (220 lb⋅in.)i + (528 lb⋅in.) j + (192 lb⋅in.)k
= (620 lb⋅in.)i + (1488 lb⋅in.) j + (192 lb⋅in.)k
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
continued
- 75. COSMOS: Complete Online Solutions Manual Organization System
( )2 ( )2 ( )2 M = 620 + 1488 + 192 lb⋅in.
= 1623.39 lb⋅in.
M ⋅ i + ⋅ j + ⋅
k λ
= =
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or M = 1.623 kip⋅in.W
(620 lb in.) (1488 lb in.) (192 lb in.)
M 1623.39 lb ⋅
in.
= 0.38192i + 0.91660 j + 0.118271k
cosθ x = 0.38192 or θ x = 67.5° W
cosθ y = 0.91660 or θ y = 23.6° W
cosθ z = 0.118271 or θ z = 83.2°W
- 76. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 74.
Have M = M1 + M2
Where M1 = rE/D × FD
= −(0.7 m)k × (80 N) j
= (56.0 N⋅m)i
And M2 = rG/F × FB
Now ( )2 ( )2 ( )2 dBF = −0.300 m + 0.540 m + 0.350 m
= 0.710m
Then FB = λBFFB
( − 0.300 m) i + (0.540 m) j +
(0.350 m) k
( 71 N
)
0.710 m
=
= −(30 N)i + (54 N) j + (35 N)k
∴ ( ) ( ) ( ) ( ) M2 = 0.54 m j × − 30 N i + 54 N j + 35 N k
= (18.90 N⋅m)i + (16.20 N⋅m)k
Finally M = (56.0 N⋅m)i + (18.90 N⋅m)i + (16.20 N⋅m)k
= (74.9 N⋅m)i + (16.20 N⋅m)k
and ( )2 ( )2 M = 74.9 N⋅m + 16.20 N⋅m
= 76.632 N⋅m or M = 76.6 N⋅m W
cos 74.9 cos 0 cos 16.20
x 76.632 y 76.632 z 76.632 θ = θ = θ =
or θ x = 12.20° θ y = 90.0° θ z = 77.8° W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 77. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 75.
Have M = (M1 + M2 ) + MP
From the solution to Problem 3.74
( ) ( ) ( ) M1 + M2 = 74.9 N⋅m i + 16.20 N⋅m k
Now MP = rD / E × PE
= (0.54 m) j + (0.70 m)k × (90 N)i
= (63.0 N⋅m) j − (48.6 N⋅m)k
∴ M = (74.9i + 16.20k) + (63.0 j − 48.6 k)
= (74.9 N⋅m)i + (63.0 N⋅m) j − (32.4 N⋅m)k
and ( )2 ( )2 ( )2 M = 74.9 N⋅m + 63.0 N⋅m + −32.4 N⋅m
= 103.096 N⋅m
−
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or M = 103.1 N⋅m W
and cos 74.9 cos 63.0 cos 32.4
θ x = θ 103.096 y = θ
=
103.096 z 103.096 or θ x = 43.4° θ y = 52.3° θ z = 108.3° W
- 78. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 76.
Have M = M1 + M2 + MP
From Problem 3.73 solution:
( ) ( ) M1 = 400 lb⋅in. i + 960 lb⋅in. j
( ) ( ) ( ) M2 = 220 lb⋅in. i + 528 lb⋅in. j + 192 lb⋅in. k
Now MP = rE/A × PE
( ) ( ) ( ) rE/A = 19.2 in. i + 8 in. j − 44 in. k
PE = (52.5 lb) j
Therefore
i j k
19.2 8 44
0 52.5 0
P = −
M
= (2310 lb. in.)i + (1008 lb. in.)k
and M = M1 + M2 + MP
= [(400 + 220 + 2310)i + (960 + 528)j + (192 +1008)k] lb⋅in.
= (2930 lb⋅in.)i + (1488 lb⋅in.) j + (1200 lb⋅in.)k
( )2 ( )2 ( )2 M = 2930 + 1488 + 1200
= 3498.4 lb⋅in.
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or M = 3.50 kip⋅in.W
continued
- 79. COSMOS: Complete Online Solutions Manual Organization System
M 2930 i + 1488 j +
= = 1200
k
M
3498.4
λ
= 0.83753i + 0.42534j + 0.34301k
cosθ x = 0.83753
or θ x = 33.1° W
cosθ y = 0.42534
or θ y = 64.8° W
cosθ z = 0.34301
or θ z = 69.9° W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 80. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 77.
Have M = M1 + M2 + M3
Where M1 = −(1.2 lb⋅ft)cos 25°j − (1.2 lb⋅ft)sin 25°k
M2 = −(1.3 lb⋅ft) j
M3 = −(1.4 lb⋅ft)cos 20°j + (1.4 lb⋅ft)sin 20°k
∴ M = (−1.08757 − 1.3 − 1.31557) j + (−0.507142 + 0.478828)k
= −(3.7031 lb⋅ft) j − (0.028314 lb⋅ft)k
and ( )2 ( )2 M = −3.7031 + −0.028314 = 3.7032 lb⋅ft
− −
= M = j k
M
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or M = 3.70 lb⋅ft W
3.7031 0.028314
3.7032
λ
= −0.99997j − 0.0076458k
cosθ x = 0
or θ x = 90°W
cosθ y = −0.99997
or θ y = 179.6° W
cosθ z = −0.0076458
or θ z = 90.4° W
- 81. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 78.
(a) FB = P: ∴ FB = 160.0 N 50.0° W
MB = −rBAPcos10°
= −(0.355 m)(160 N)cos10°
= −55.937 N⋅m
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or MB = 55.9 N⋅m W
(b) FC = P: ∴ FC = 160.0 N 50.0° W
( ) C B CB B M M r F⊥
= −
= MB − rCBFB sin 55°
= −55.937 N⋅m − (0.305 m)(160 N)sin 55°
or MC = 95.9 N⋅m W
- 82. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 79.
(a) ΣF: FB = 135 N
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or FB = 135 N W
ΣM: MB = P dB
= (135 N)(0.125 m)
= 16.875 N⋅m
or MB = 16.88 N⋅m W
(b) ΣMB : MB = FC d
16.875 N⋅m = FC (0.075 m)
FC = 225 N
or FC = 225 N W
ΣF: 0 = − FB + FC
FB = FC = 225 N
or FB = 225 N W
- 83. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 80.
(a) Based on ΣF: PC = P = 700 N
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or PC = 700 N 60°W
ΣMC : MC = −PxdCy + PydCx
where Px = (700 N)cos60° = 350 N
Py = (700 N)sin 60° = 606.22 N
dCx = 1.6 m
dCy = 1.1 m
∴ MC = −(350 N)(1.1 m) + (606.22 N)(1.6 m)
= −385 N⋅m + 969.95 N⋅m
= 584.95 N⋅m
or MC = 585 N⋅m W
(b) Based on ΣFx : PDx = Pcos60°
= (700 N)cos60°
= 350 N
ΣMD : (Pcos60°)(dDA ) = PB (dDB )
(700 N)cos60° (0.6 m) = PB (2.4 m)
PB = 87.5 N
or PB = 87.5 N W
- 84. COSMOS: Complete Online Solutions Manual Organization System
ΣFy : Psin 60° = PB + PDy
(700 N)sin 60° = 87.5 N + PDy
PDy = 518.72 N
( ) ( )2 2
PD = PDx + PDy
( )2 ( )2 = 350 + 518.72 = 625.76 N
P
P
θ = tan − 1 = tan − 1 518.72 = 55.991
°
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
350
Dy
Dx
or PD = 626 N 56.0°W
- 85. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 81.
ΣFx : 2.8cos65° = FA cosθ + FC cosθ
= (FA + FC )cosθ (1)
ΣFy : 2.8sin 65° = FA sinθ + FC sinθ
= (FA + FC )sinθ (2)
Then (2) tan 65 tan
(1)
⇒ ° = θ
or θ = 65.0°
ΣMA : (27 m)(2.8 kN)sin 65° = (72 m)(FC )sin 65°
or FC = 1.050 kN
From Equation (1): 2.8 kN = FA + 1.050 kN
or FA = 1.750 kN
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
∴ FA = 1.750 kN 65.0°W
FC = 1.050 kN 65.0° W
- 86. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 82.
Based on
ΣFx : − (54 lb)cos30° = −FB cosα − FC cosα
(FB + FC )cosα = (54 lb)cos30° (1)
ΣFy : (54 lb)sin 30° = FB sinα + FC sinα
or (FB + FC )sinα = (54 lb)sin 30° (2)
From ( )
2
: tan tan30
1
( )
Eq
Eq
α = °
∴α = 30°
Based on ΣMC : (54 lb)cos(30° − 20°) (10 in.) = (FB cos10°)(24 in.)
∴ FB = 22.5 lb
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or FB = 22.5 lb 30° W
From Eq. (1), (22.5 + FC )cos30° = (54)cos30°
FC = 31.5 lb
or FC = 31.5 lb 30° W
- 87. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 83.
(a) Based on
ΣFx : −(54 lb)cos30° = − FC cos30°
∴ FC = 54 lb
1 27 : tan 63.006
2 13.7534
27 30.301 lb
B sin 63.006 F = =
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or FC = 54.0 lb 30° W
ΣMC : (54 lb)cos10° (10 in.) = MC
∴ MC = 531.80 lb⋅in.
or MC = 532 lb⋅in. W
(b) Based on
ΣFy : (54 lb)sin 30° = FB sinα
or FB sinα = 27 (1)
ΣMB : 531.80 lb⋅in. − (54 lb)cos10° (24 in.)
= − FC (24 in.)cos 20°
FC = 33.012 lb
or FC = 33.0 lb W
And ΣFx : −(54 lb)cos30° = −33.012 lb − FB cosα
FB cosα = 13.7534 (2)
From ( )
( )
Eq
Eq
α = ∴α = °
From Eq. (1), ( °
)
or FB = 30.3 lb 63.0° W
- 88. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 84.
ΣF F + F + F = F
(a) Have :
y C D E
F = −200lb + 150 lb − 150 lb
F = −200 lb
ΣM F d − − F =
(200 lb)(d − 4.5 ft ) − (150 lb)(6 ft ) = 0
ΣM F d − + F =
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or F = 200 lb
Have : ( 4.5 ft ) (6 ft ) 0
G C D
d = 9 ft
or d = 9.00 ft
(b) Changing directions of the two 150-lb forces only changes the sign of
the couple.
∴ F = −200 lb
or F = 200 lb
And : ( 4.5 ft ) (6 ft ) 0
G C D
(200 lb)(d − 4.5 ft ) + (150 lb)(6 ft ) = 0
d = 0
or d = 0
- 89. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 85.
(a)
(b)
(c)
Based on ΣFz :
−200 N + 200 N + 240 N = FA
FA = 240 N
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or FA = (240 N)k W
Based on ΣMA:
(200 N)(0.7 m) − (200 N)(0.2 m) = MA
MA = 100 N⋅m
or MA = (100.0 N⋅m) jW
Based on ΣFz :
−200 N + 200 N + 240 N = F
F = 240 N
or F = (240 N)k W
Based on ΣMA:
100 N⋅m = (240 N)(x)
x = 0.41667 m
or x = 0.417 m From A along AB W
Based on ΣMB :
−(200 N)(0.3 m) + (200 N)(0.8 m) − P(1 m) = R(0)
P = 100 N
or P = 100.0 N W
- 90. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 86.
Let R be the single equivalent force...
ΣF: R = FA + FC
= (260 N)(cos10°i − sin10°k) + (320 N)(−cos8°i − sin8°k)
= −(60.836 N)i − (89.684 N)k
or R = −(60.8 N)i − (89.7 N)k W
ΣMA : rADRx = rACFC cos8°
rAD (60.836 N) = (0.690 m)(320 N)cos8°
rAD = 3.5941 m
∴R Would have to be applied 3.59 m to the right of A W
on an extension of handle ABC.
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 91. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 87.
(a) Have ΣF: FB + FC + FD = FA
Since FB = −FD
∴ FA = FC = 22 lb 20°
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or FA = 22.0 lb 20° W
Have ΣMA : − FBT (r ) − FCT (r ) + FDT (r ) = MA
− (28 lb)sin15° (8 in.) − (22 lb)sin 25° (8 in.)
+ (28 lb)sin 45° (8 in.) = MA
MA = 26.036 lb⋅in.
or MA = 26.0 lb⋅in. W
(b) Have ΣF: FA = FE
or FE = 22.0 lb 20° W
ΣM: MA = [FE cos 20°](a)
∴ 26.036 lb⋅in. = (22 lb)cos 20° (a)
a = 1.25941 in.
or a = 1.259 in. Below AW
- 92. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 88.
(a) Let R be the single equivalent force. Then
R = (120 N)k R = 120 N W
ΣMB : − a(120 N) = −(0.165 m)(90 N)cos15° + (0.201 m)(90 N)sin15°
a = 0.080516 m
∴The line of action is y = 201mm − 80.516 mm =
19.984 mm
2
2 3.1697 3.1697 4 2.48396 0.69263
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or y = 19.98 mm W
(b) ΣMB : − (0.201 − 0.040)m (120 N) = −(0.165 m)(90 N)cosθ + (0.201 m)(90 N)sinθ
or cosθ − 1.21818sinθ = 1.30101
or cos2θ = (1.30101 + 1.21818sinθ )2
or 1 − sin2θ = 1.69263 + 3.1697sinθ + 1.48396sin2θ
or 2.48396sin2θ + 3.1697sinθ + 0.69263 = 0
Then
( ) ( )( )
( )
sin
2 2.48396
θ
− ± −
=
or θ = −16.26° and θ = −85.0° W
- 93. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 89.
(a) First note that F = P and that F must be equivalent to (P, MD) at point D,
Where MD = 57.6 N⋅m
For ( )min F = F F must act as far from D as possible
∴ Point of application is at point B W
(b) For ( )min F F must be perpendicular to BD
Now ( )2 ( )2 dDB = 630 mm + −160 mm
= 650 mm
tan 63
16
α =
α = 75.7°
Then MD = dDB F
57.6 N⋅m = (0.650 m)F
F = 88.6 N
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or F = 88.6 N 75.7°W
- 94. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 90.
Have ΣF: −(250 kN) j = F
i j k
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or F = −(250 kN) jW
Also have ΣMG : rP × P = M
0.030 0 0.060 kN m =
0 250 0
− ⋅
−
M
∴ M = (15 kN⋅m)i + (7.5 kN⋅m)k
or M = (15.00 kN⋅m)i + (7.50 kN⋅m)k W
- 95. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 91.
Have ΣF: TAB = F
JJJG
T AB
T =
where AB AB
AB
i j k
54 lb 2.25 18 9
( )
− +
( 2.25 )2 ( 18 )2 ( 9
)2
=
+ − +
= (6 lb)i − (48 lb) j + (24 lb)k
So that F = (6.00 lb)i − (48.0 lb) j + (24.0 lb)k W
Have ΣME : rA/E × TAB = M
i j k
0 22.5 0 lb ft
6 48 24
⋅ =
−
M
∴M = (540 lb⋅ft)i − (135 lb⋅ft)k
or M = (540 lb⋅ft)i − (135.0 lb⋅ft)k W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 96. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 92.
Have ΣF: TCD = F
JJJG
T CD
T =
where CD CD
CD
i j k
61 lb 0.9 16.8 7.2
( )
− − +
( 0.9 )2 ( 16.8 )2 ( 7.2
)2
=
− + − +
= −(3 lb)i − (56 lb) j + (24 lb)k
So that F = −(3.00 lb)i − (56.0 lb) j + (24.0 lb)k W
Have ΣMO = rC/D × TCD = M
i j k
0 22.5 0 lb ft
3 56 24
⋅ =
− −
M
∴M = (540 lb⋅ft)i + (67.5 lb⋅ft)k
M = (540 lb⋅ft)i + (67.5 lb⋅ft)k W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 97. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 93.
Have ΣF: TAB = F
JJJG
T AB
T =
where AB AB
AB
i j k
10.5 kN 4.75 2
( )
− − +
( 1 )2 ( 4.75 )2 ( 2
)2
=
− + − +
= −(2 kN)i − (9.5 kN) j + (4 kN)k
So that F = −(2.00 kN)i − (9.50 kN) j + (4.00 kN)k W
Have ΣMO : rA × TAB = M
i j k
3 4.75 0 kNm
2 9.5 4
⋅ =
− −
M
∴M = (19 kN⋅m)i − (12 kN⋅m) j − (19 kN⋅m)k
M = (19.00 kN⋅m)i − (12.00 kN⋅m) j − (19.00 kN⋅m)k W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 98. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 94.
Let (R, MO ) be the equivalent force-couple system
Then R = (220 N)(−sin 60°j − cos60°k)
= (110 N)(− 3j − k)
or R = −(190.5 N) j − (110 N)k W
Now ΣMO : MO = rOC × R
Where rOC = (0.2 m)i + (0.1 − 0.4sin 20°)m j + (0.4cos 20°m)k
i j k
Then (0.1)(110 N) 2 (1 4sin 20 ) 4cos 20 (m)
O = − − ° °
0 3 1
M
= −(11 N⋅m){(1 − 4sin 20°)(1) − (4cos 20°)( 3) i − 2 j + 2 3 k}
or MO = (75.7 N⋅m)i + (22.0 N⋅m) j − (38.1 N⋅m)k W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 99. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 95.
Have ΣF: F = FD
JJG
where F AI
AI
F =
i j k
63 lb 14.4 4.8 7.2
( )
− +
( 14.4 )2 ( 4.8 )2 ( 7.2
)2
=
+ − +
So that F = (54.0 lb)i − (18.00 lb) j + (27.0 lb)k W
Have ΣMD : M + rI/O × F = MD
JJJG
where M AC
AC
M =
i k
560 lb in. 9.6 7.2
( )
−
( 9.6 )2 ( 7.2
)2
= ⋅
+ −
= (448 lb⋅in.)i − (336 lb⋅in.)k
i j k
Then (448 lb in.) (336 lb in.) 0 0 14.4 lb in.
D = ⋅ − ⋅ + ⋅
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
54 −
18 27
M i k
= (448 lb⋅in.)i − (336 lb⋅in.)k + (259.2 lb⋅in.)i + (777.6 lb⋅in.) j
or MD = (707 lb⋅in.)i + (778 lb⋅in.) j − (336 lb⋅in.)k W
- 100. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 96.
First assume that the given force W and couples M1 and M2 act at the
origin.
Now W = −Wj
and M = M1 + M2 = −(M2 cos 25°)i + (M1 − M2 sin 25°)k
Note that since W and M are perpendicular, it follows that they can be
replaced with a single equivalent force.
(a) Have F = W or F = −Wj = −(2.4 N) j
i j k
x z Wz Wx
= = −
W
−
= − ° = − − °
x = − ° = −
z = − ° = −
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or F = −(2.40 N) j W
(b) Assume that the line of action of F passes through point P (x, 0, z).
Then for equivalence
M = rP/O × F
where rP/O = xi + zk
∴ −(M2 cos 25°)i + (M1 − M2 sin 25°)k
0 ( ) ( )
0 0
i k
Equating the i and k coefficients,
z Mz cos 25 and x M1 M2 sin 25
W W
(b) For W = 2.4 N, M1 = 0.068 N⋅m, M2 = 0.065 N⋅m
0.068 0.065sin 25 0.0168874 m
2.4
−
or x = −16.89 mmW
0.065cos 25 0.024546 m
2.4
or z = −24.5 mmW
- 101. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 97.
(a) Have ΣMBz : M2z = 0
( ) k⋅ rH/B × F1 + M1z = 0 (1)
where ( ) ( ) rH/B = 31 in. i − 2 in. j
F1 = λEHF1
(6 in.) + (6 in.) −
(7 in.) ( )
i j k
− + −
= ⋅
⋅ − ⋅
− + =
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
20 lb
11.0 in.
=
i j k
20 lb (6 6 7 )
11.0
= i + j − k
M1z = k⋅M1
M1 = λEJM1
( 3 in. ) ( 7 in.
) ( 480 lb in.
) 2
58 in.
d
d
+
Then from Equation (1),
( )( )
2
0 0 1
20 lb in. 7 480 lb in. 31 2 0 0
11.0 6 6 − 7 d
+
58 continued
- 102. COSMOS: Complete Online Solutions Manual Organization System
Solving for d, Equation (1) reduces to
20 lb ⋅ in. ( ⋅
186 + 12 ) − 3360 lb in. =
0
11.0 d 2
+
58
From which d = 5.3955 in.
or d = 5.40 in.W
20 lb 6 6 7
11.0
(b) F 2 = F 1
= ( i + j − k
) = (10.9091i + 10.9091j − 12.7273k)lb
( ) ( ) ( ) or F2 = 10.91 lb i + 10.91 lb j − 12.73 lb k W
M2 = rH/B × F1 + M1
i j k
⋅ ( − 5.3955) i + 3 j −
7 k
31 2 0 20 lb in. (480 lb in.)
= − + ⋅
11.0 9.3333
6 6 −
7
= (25.455i + 394.55j + 360k)lb⋅in.
+(−277.48i + 154.285j − 360k)lb⋅in.
( ) ( ) M2 = − 252.03 lb⋅in. i + 548.84 lb⋅in. j
( ) ( ) or M2 = − 21.0 lb⋅ft i + 45.7 lb⋅ft j W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 103. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 98.
(a) a: ΣFy : Ra = −400 N − 600 N
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or Ra = 1000 N W
ΣMB : Ma = (2 kN⋅m) + (2 kN⋅m) + (5 m)(400 N)
or Ma = 6.00 kN⋅m W
b: ΣFy : Rb = −1200 N + 200 N
or Rb = 1000 N W
ΣMB : Mb = (0.6 kN⋅m) + (5 m)(1200 N)
or Mb = 6.60 kN⋅m W
c: ΣFy : Rc = 200 N − 1200 N
or Rc = 1000 N W
ΣMB : Mc = −(4 kN⋅m) − (1.6 kN⋅m) − (5 m)(200 N)
or Mc = 6.60 kN⋅m W
d : ΣFy : Rd = −800 N − 200 N
or Rd = 1000 N W
ΣMB : Md = −(1.6 kN⋅m) + (4.2 kN⋅m) + (5 m)(800 N)
or Md = 6.60 kN⋅m W
continued
- 104. COSMOS: Complete Online Solutions Manual Organization System
e: ΣFy : Re = −500 N − 400 N
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or Re = 900 N W
ΣMB : Me = (3.8 kN⋅m) + (0.3 kN⋅m) + (5 m)(500 N)
or Me = 6.60 kN⋅m W
f : ΣFy : Rf = 400 N − 1400 N
or R f = 1000 N W
ΣMB : M f = (8.6 kN⋅m) − (0.8 kN⋅m) − (5 m)(400 N)
or Mf = 5.80 kN⋅m W
g: ΣFy : Rg = −1200 N + 300 N
or Rg = 900 N W
ΣMB : Mg = (0.3 kN⋅m) + (0.3 kN⋅m) + (5 m)(1200 N)
or Mg = 6.60 kN⋅m W
h: ΣFy : Rh = −250 N − 750 N
or Rh = 1000 N W
ΣMB : Mh = −(0.65 kN⋅m) + (6 kN⋅m) + (5 m)(250 N)
or Mh = 6.60 kN⋅m W
(b) The equivalent loadings are (b), (d), (h) W
- 105. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 99.
The equivalent force-couple system at B is...
ΣFy : R = −650 N − 350 N
or R = 1000 N
ΣMB : M = (1.6 m)(800 N) + (1.27 kN⋅m) + (5 m)(650 N)
or M = 5.80 kN⋅m
∴ The equivalent loading of Problem 3.98 is (f) W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 106. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 100.
Equivalent force system...
(a) ΣFy : R = −400 N − 200 N
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or R = 600 N W
ΣMA : −d (600 N) = −(200 N⋅m) + (100 N⋅m) − (4 m)(200 N)
or d = 1.500 m W
(b) ΣFy : R = −400 N + 100 N
or R = 300 N W
ΣMA : −d (300 N) = −(200 N⋅m) − (600 N⋅m) + (4 m)(100 N)
or d = 1.333 m W
(c) ΣFy : R = −400 N − 100 N
or R = 500 N W
ΣMA : −d (500 N) = −(200 N⋅m) − (200 N⋅m) − (4 m)(100 N)
or d = 1.600 m W
- 107. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 101.
The equivalent force-couple system at A for each of the five force-couple systems will be determined and
compared to
F = (2 lb) j M = (48 lb⋅in.)i + (32 lb⋅in.)k
To determine if they are equivalent
Force-couple system at B:
Have ΣF: F = (2 lb) j
and ( ) ΣMA : M = ΣMB + rB/A × FB
M = (32 lb⋅in.)i + (16 lb⋅in.)k + (8 in.)i × (2 lb) j
= (32 lb⋅in.)i + (32 lb⋅in.)k
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
∴ is not equivalent W
Force-couple system at C:
Have ΣF: F = (2 lb) j
And ( ) ΣMA : M = MC + rC/A × FC
M = (68 lb⋅in.)i + (8 in.)i + (10 in.)k × (2 lb) j
= (48 lb⋅in.)i + (16 lb⋅in.)k
∴ is not equivalent W
continued
- 108. COSMOS: Complete Online Solutions Manual Organization System
Force-couple system at E:
Have ΣF: F = (2 lb) j
and ( ) ΣMA : M = ME + rE/A × FE
M = (48 lb⋅in.)i + (16 in.)i − (3.2 in.) j × (2 lb) j
= (48 lb⋅in.)i + (32 lb⋅in.)k
∴ is equivalent W
Force-couple system at G:
Have ΣF: F = (2 lb)i + (2 lb) j
F has two force components
∴ is not equivalent W
Force-couple system at I:
Have ΣF: F = (2 lb) j
and ( ) ΣMA : ΣMI + rI/A × FI
M = (80 lb⋅in.)i − (16 in.)k
+ (16 in.)i − (8 in.) j + (16 in.)k × (2 lb) j
M = (48 lb⋅in.)i + (16 lb⋅in.)k
∴ is not equivalent W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 109. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 102.
First WA = mAg = (38 kg) g
WB = mBg = (29 kg) g
(a) WC = mCg = (27 kg) g
For resultant weight to act at C, ΣMC = 0
Then (38 kg) g (2 m) − (27 kg) g (d ) − (29 kg) g (2 m) = 0
76 58 0.66667 m
27
d −
∴ = =
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or d = 0.667 m W
(b) WC = mCg = (24 kg) g
For resultant weight to act at C, ΣMC = 0
Then (38 kg) g (2 m) − (24 kg) g (d ) − (29 kg) g (2 m) = 0
76 58 0.75 m
24
d −
∴ = =
or d = 0.750 m W
- 110. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 103.
ΣF −W − W − W = R
∴R = −200 lb − 175 lb − 135 lb
(a) Have :
C D E
= −510 lb
Σ =−
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or R = 510 lb
Have :
A
ΣM
−(200 lb)(4.5 ft ) − (175 lb)(7.8 ft ) − (135 lb)(12.75 ft ) = − R(d )
∴−3986.3 lb⋅ft = (−510 lb)d
or d = 7.82 ft
(b) For equal reactions at A and B,
The resultant R must act at midspan.
From
2
A
L
M R
∴−(200 lb)(4.5 ft ) − (175 lb)(4.5 ft + a) − (135 lb)(4.5 ft + 2.5 a)
= −(510 lb)(9 ft )
or 2295 + 512.5 a = 4590
and a = 4.48 ft
- 111. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 104.
Have ΣF: −12 kN − WL − 18 kN = −40 kN − 40 kN
WL = 50 kN
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or WL = 50.0 kN W
ΣMB : (12 kN)(5 m) + (50 kN)d = (40 kN)(5 m)
d = 2.8 m
or heaviest load (50 kN) is located W
2.80 m from front axle
- 112. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 105.
(a) ΣF: R = (80 N)i − (40 N) j − (60 N) j +(90 N)(−sin 50°i − cos50°j)
= (11.0560 N)i − (157.851 N) j
( )2 ( )2 R = 11.0560 N + −157.851 N
= 158.2 N
−
tan =
157.851
11.0560
θ
θ = 86.0°
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or R = 158.2 N 86.0° W
(b)
ΣMF : d −(157.851 N) = (0.32 m)(80 N) − (0.15 m)(40 N) − (0.35 m)(60 N)
− (0.61 m)(90 N)cos50° − (0.16 m)(90 N)sin 50°
or d = 302 mm to the right of F W
- 113. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 106.
(a) : 0 (0.32 m)(80 N) (0.1 m)(40 N) (0.1 m)(60 N) (0.36 m)(90 N)cos
ΣM = + − − α
I
−(0.16 m)(90 N)sinα
or 4sinα + 9cosα = 6.5556
( ) ( ) 2 2
9cosα = 6.5556 − 4sinα
( 2 ) 2 81 1 − sin α = 42.976 − 52.445sinα + 16sin α
2 97sin α − 52.445sinα − 38.024 = 0
Solving by the quadratic formula gives for the positive root
sinα = 0.95230
α = 72.233°
or α = 72.2°
Note: The second root (α = −24.3°) is rejected since 0 α 90°.
(b) ΣF: R = (80 N)i − (40 N) j − (60 N) j
+(90 N)(−sin 72.233°i − cos72.233°j)
= −(5.7075 N)i − (127.463 N) j
( ) ( ) 2 2
R = −5.7075 N + −127.463 N
= 127.6 N
127.463
θ = −
tan
5.7075
−
θ = 87.4°
or R = 127.6 N 87.4°
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 114. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 107.
(a) Have ΣMD : 0 = M − (0.8 in.)(40 lb) − (2.9 in.)(20 lb)cos30° −(3.3 in.)(20 lb)sin 30°
or M = 115.229 lb⋅in.
or M = 115.2 lb⋅in. W
Now, R is oriented at 45° as shown (since its line of action
passes through B and D).
Have ΣFx′ : 0 = (40 lb)cos 45° − (20 lb)cos15°
−(90 lb)cos(α + 45°)
or α = 39.283°
or α = 39.3° W
(b) ΣFx : Rx = 40 − 20sin 30° − 90cos39.283°
= −39.663 lb
Now R = 2Rx or R = 56.1 lb 45.0° W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 115. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 108.
(a) Reduce system to a force and couple at B:
Have R = ΣF = −(10 lb) j + (25 lb)cos60°i + (25 lb)sin 60°j − (40 lb)i
= −(27.5 lb)i + (11.6506 lb) j
or ( )2 ( )2 R = −27.5 lb + 11.6506 lb = 29.866 lb
tan 1 11.6506 22.960
θ = − = °
27.5
or R = 29.9 lb 23.0° W
Also MB = ΣMB = (80 lb⋅in.)k − (12 in.)i × (−10 lb) j − (8 in.) j × (−40 lb)i
= −(120 lb⋅in.)k
(b)
Have MB = −(120 lb⋅in.)k = −(u)i × (11.6506 lb) j
−(120 lb⋅in.)k = −(11.6506 lb)(u)k
u = 10.2999 in. and x = 12 in. − 10.2999 in.
= 1.7001 in.
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 116. COSMOS: Complete Online Solutions Manual Organization System
Have MB = −(120 lb⋅in.)k = −(v) j × (−27.5 lb)i
−(120 lb⋅in.)k = −(27.5 lb)(v)k
v = 4.3636 in.
and y = 8 in. − 4.3636 in. = 3.6364 in.
or 1.700 in. to the right of A and 3.64 in. above C W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 117. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 109.
(a) Position origin along centerline of sheet metal at the intersection with
line EF.
(a) Have ΣF = R
R = −0.52 j − 1.05 j − 2.1(sin 45°i + cos 45° j) − 0.64i kips
R = −(2.1249 kips)i − (3.0549 kips) j
( ) ( ) 2 2
R = −2.1249 + −3.0549
= 3.7212 kips
− − 3.0549
θ = 1 tan = 55.179
° − 2.1249
or R = 3.72 kips 55.2°
M = ΣM
Have EF EF
Where M = (0.52 kip)(3.6 in.) +
(1.05 kips)(1.6 in.) EF
−(2.1 kips)(0.8 in.) − (0.64 kip)(1.6 in.)sin 45° + 1.6 in.
= 0.123923 kip⋅in.
To obtain distance d left of EF,
Have M = dR = d ( −
3.0549 kips) EF y
0.123923 kip ⋅ in.
d = = −
0.040565 in.
3.0549 kips
−
or d = 0.0406 in. left of EF
(b)
M = ΣM =
Have 0
EF EF
(0.52 kip)(3.6 in.) (1.05 kips)(1.6 in.) EF
M = +
−(2.1 kips)(0.8 in.)
−(0.64 kip)(1.6 in.)sinα + 1.6 in.
∴ (1.024 kip⋅in.)sinα = 0.848 kip⋅in.
or α = 55.9°
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 118. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 110.
(a) Have ΣF = R
R = −0.52j − 1.05j − 2.1(sinαi + cosα j) − 0.64i kips
= − 0.64 kip + (2.1 kips)(sinα )i − 1.57 kips + (2.1 kips)cosα j
R
R
Then tan 0.64 2.1sin
α
+
1.57 2.1cos
x
y
α
α
= =
+
1.57 tanα + 2.1sinα = 0.64 + 2.1sinα
tan 0.64
1.57
α =
α = 22.178°
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or α = 22.2° W
(b) From α = 22.178°
Rx = −0.64 kip − (2.1 kips)sin 22.178°
= −1.43272 kips
Ry = −1.57 kips − (2.1 kips)cos 22.178°
= −3.5146 kips
- 119. COSMOS: Complete Online Solutions Manual Organization System
( )2 ( )2 R = −1.43272 + −3.5146
= 3.7954 kips
or R = 3.80 kips 67.8°W
Then MEF = ΣMEF
Where MEF = (0.52 kip)(3.6 in.) + (1.05 kips)(1.6 in.) − (2.1 kips)(0.8 in.)
−(0.64 kip)(1.6 in.)sin 22.178° + 1.6 in.
= 0.46146 kip⋅in.
To obtain distance d left of EF,
Have MEF = dRy
= d (−3.5146 kips)
0.46146 kip in.
d ⋅
3.5146 kips
=
−
= −0.131298 in.
or d = 0.1313 in. left of EF W
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
- 120. COSMOS: Complete Online Solutions Manual Organization System
Chapter 3, Solution 111.
Equivalent force-couple at A due to belts on pulley A
Have ΣF: −120 N − 160 N = RA
∴ RA = 280 N
Have ΣMA : −40 N(0.02 m) = MA
∴ MA = 0.8 N⋅m
Equivalent force-couple at B due to belts on pulley B
Have ΣF: (210 N + 150 N) 25° = RB
∴ RB = 360 N 25°
Have ΣMB : −60 N(0.015 m) = MB
∴ MB = 0.9 N⋅m
Equivalent force-couple at F
Have ΣF: RF = (−280 N) j + (360 N)(cos 25°i + sin 25°j)
= (326.27 N)i − (127.857 N) j
R = RF = RF2x + RF2y = (326.27)2 + (127.857)2 = 350.43 N
R
R
− θ = tan − 1 = tan − 1 127.857 = − 21.399
°
326.27
Fy
Fx
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or RF = R = 350 N 21.4°W
- 121. COSMOS: Complete Online Solutions Manual Organization System
Have
ΣMF : MF = −(280 N)(0.06 m) − 0.80 N⋅m
− (360 N)cos 25° (0.010 m)
+ (360 N)sin 25° (0.120 m) − 0.90 N⋅m
MF = −(3.5056 N⋅m)k
To determine where a single resultant force will intersect line FE,
MF = dRy
3.5056 N m 0.027418 m 27.418 mm
127.857 N
F
y
d M
∴ = = = =
R
− ⋅
−
Vector Mechanics for Engineers: Statics and Dynamics, 8/e, Ferdinand P. Beer, E. Russell Johnston, Jr.,
Elliot R. Eisenberg, William E. Clausen, David Mazurek, Phillip J. Cornwell
© 2007 The McGraw-Hill Companies.
or d = 27.4 mmW