Chapter 8 8 Rotational Equilibrium and Rotational Dynamics PROBLEM SOLUTIONS 8.1 Since the friction force is tangential to a point on the rim of the wheel, it is perpendicular to the radius line connecting this point with the center of the wheel. The torque of this force about the axis through the center of the wheel is then = rf sin 90.0º = rf, and the friction force is f 8.2 r 76.0 N m 217 N 0.350 m The torque of the applied force is = rF sin. Thus, if r = 0.330 m, = 75.0º, and the torque has the maximum allowed value of max = 65.0 N m, the applied force is F 8.3 max 65.0 N m 204 N r sin 0.330 m sin 75.0 First resolve all of the forces shown in Figure P8.3 into components parallel to and perpendicular to the beam as shown in the sketch below. Page 8.1 Chapter 8 (a) O 25 N cos 30 2.0 m 10 N sin 20 4.0 m 30 N m or (b) C 30 N sin 45 2.0 m 10 N sin 20 2.0 m 36 N m or 8.4 0 = 30 N m counterclockwise c = 30 N m counterclockwise The lever arm is d 1.20 102 m cos 48.0 8.03 103 m , and the torque is Fd 80.0 N 8.03 103 m 0.642 N m counterclockwise 8.5 (a) Fg lever arm mg sin 3.0 kg 9.8 m s2 2.0 m sin 5.0 5.1 N m (b) The magnitude of the torque is proportional to the sin , where is the angle between the direction of the force and the line from the pivot to the point where the force acts. Note from the sketch that this is the same as the an gle the pendulum string makes with the vertical. Since sin increases as increases, the torque also increases with the angle. 8.6 The object is in both translational and rotational equilibrium. Thus, we may write: Fx 0 Fx Rx 0 Fy 0 Fy Ry Fg 0 and Page 8.2 Chapter 8 O 0 Fy cos Fx sin Fg cos 0 2 8.7 Requiring that = 0, using the shoulder joint at point O as a pivot, gives Ft sin12.0 0.080 m 41.5 N 0.290 m 0 or Ft 724 N Then Fy 0 Fsy 724 N sin12.0 41.5 N = 0 , yielding Fsy 109 N Fy 0 gives Fsx 724 N cos12.0 = 0 , or Fsx 708 N Therefore, Fs 8.8 (a) Fsx2 Fsy2 708 N 2 109 N 2 716 N Since the beam is in equilibrium, we choose the center as our pivot point and require that center FSam 2.80 m FJoe 1.80 m 0 or FJoe 1.56FSam [1] Also, Fy 0 FSam FJoe 450 N [2] Substitute Equation [1] into [2] to get the following: FSam 1.56FSam 450 N or FSam Page 8.3 450 N 176 N 2.56 Chapter 8 Then, Equation [1] yields FJoe 1.56 176 N 274 N . (b) If Sam moves closer to the center of the beam, his lever arm about the beam center decreases, so the force FSam must increase to continue applying a clockwise torque capable of offsetting Joe’s counterclockwise torque. At the same time, the force FJoe would decrease since the sum of the two upward forces equal the magnitude of the downward gravitational force. (c) If Sam moves to the right of the center of the beam, his torque about the midpoint would then be counterclockwise. Joe would have to hold down on the beam in order to exert an offsetting clockwise torque. 8.9 Require that = 0 about an axis through the elbow and perpendicular to the page. This gives 2.00 kg 9.80 m s2 25.0 cm + 8.00 cm FB cos 75.0 8.00 cm 0 or FB 8.10 19.6 N 33.0 cm 8.00 cm cos 75.0 312 N Since the bare meter stick balances at the 49.7 cm mark when placed on the fulcrum, the center of gravity of the meter stick is located 49.7 cm from the zero end. Thus, the entire weight of the meter stick may be considered to be concentrated at this point. The free-body diagram of the stick when it is balanced with the 50.0-g mass attached at the 10.0 cm mark is as given at the right. Requiring that the sum of the torques about point O be zero yields 50.0 g g 39.2 cm 10.0 cm M g 49.7 cm 39.2 cm 0 or 39.2 cm 10.0 cm M 50.0 g 139 g 49.7 cm 39.2 cm Page 8.4 Chapter 8 8.11 Consider the remaining plywood to consist of two parts: A1 is a 4.00-ft-by-4.00-ft section with center of gravity located at (2.00 ft, 2.00 ft), while A2 is a 2.00-ft-by-4.00-ft section with center of gravity at (6.00 ft, 1.00 ft). Since the plywood is uniform, its mass per area is constant and the mass of a section having area A is m = A. The center of gravity of the remaining plywood has coordinates given by 6.00 ft xcg 16.0 ft 2 2.00 ft 8.00 ft 2 mi xi A1 x1 A2 x2 mi A1 A2 16.0 ft 2 8.00 ft 2 ycg 16.0 ft 2 2.00 ft 8.00 ft 2 1.00 ft mi yi A1 y1 A2 y2 1.67 ft mi A1 A2 16.0 ft 2 8.00 ft 2 3.33 ft and 8.12 (a) Mg 90.0 kg 9.80 m s2 882 N (b) mg 55.0 kg 9.80 m s2 539 N The woman is at x = 0 when n1 is greatest. With this location of the woman, the counterclockwise torque about the center of the beam is a maximum. Thus, n1 must be exerting its maximum clockwise torque about the center to hold the beam in rotational equilibrium. (c) n1 = 0 As the woman walks to the right along the beam, she will eventually reach a point where the beam will start to rotate clockwise about the rightmost pivot. At this point, the beam is starting to lift up off of the left most pivot and the normal force exerted by that pivot will have diminished to zero. (d) When the beam is about to tip, n1 = 0 and Fy = 0, gives 0+n2 – Mg – mg = 0, or n2 Mg mg 882 N 539 N 1.42 103 N Page 8.5 Chapter 8 (e) 0 when the beam is about to tip (n = 0) gives Requiring that rightmost 1 pivot 4.00 m x mg 4.00 m 3.00 m Mg 0 or mg x 1.00 m Mg 4.00 m mg , and x 1.00 m M 4.00 m m Thus, x 1.00 m (f) 90.0 kg 55.0 kg 4.00 m 5.64 m left 0 gives When n1 = 0 and n2 = 1.42 × 103 N, requiring that end 0 539 N x 882 N 3.00 m 1.42 103 N 4.00 m 0 or x 3.03 103 N m 5.62 N 539 N which, within limits of rounding errors, is the same as the answer to part (e). 8.13 Requiring that xcg mi xi mi 0 gives 5.0 kg 0 3.0 kg 0 4.0 kg 3.0 m 8.0 kg x 5.0 3.0 4.0 8.0 kg or 8.0 x + 12 m = 0 which yields x = – 1.5 m Also, requiring that ycg mi yi mi 0 gives Page 8.6 0 Chapter 8 5.0 kg 0 3.0 kg 4.0 m 4.0 kg 0 8.0 kg y 5.0 3.0 4.0 8.0 kg 0 or 8.0y + 12 m = 0 yielding y = – 1.5 m Thus, the 8.0-kg object should be placed at coordinates (–1.5 m, –1.5m) . 8.14 (a) As the woman walks to the right along the beam, she will eventually reach a point where the beam will start to rotate clockwise about the rightmost pivot. At this point, the beam is starting to lift up off of the leftmost pivot and the normal force, n1, exerted by that pivot will have diminished to zero. Then, Fy 0 0 mg Mg n2 0 , or n2 m M g (b) left 0 gives When n1 = 0 and n2 = (m + M)g, requiring that end 0 mg x Mg (c) L mg Mg 2 0 or M x 1 m M L 2m If the woman is to just reach the right end of the beam (x = L) when n1 = 0 and n2 = (m+M)g (i.e., the beam is ready to tip), then the result from Part (b) requires that M L 1 m 8.15 M L or 2m 1 M 2m 1 M m m M 2 L m M In each case, the distance from the bar to the center of mass of the body is given by xcg marms xarms mtorso xtorso mthighs xthighs mlegs xlegs mi xi mi marms mtorso mthighs mlegs where the distance x for any body part is the distance from the bar to the center of gravity of that body part. In each Page 8.7 Chapter 8 case, we shall take the positive direction for distances to run from the bar toward the location of the head. Note that mi 6.87 33.57 14.07 7.54 kg 62.05 kg . With the body positioned as shown in Figure P8.15b, the distances x for each body part is computed using the sketch given below: xarms rcg arms xtorso rcg xthighs xlegs arms arms arms 0.239 m 0.548 m + 0.337 m 0.885 m torso torso torso rcg thighs thighs 0.548 + 0.601+ 0.151 m 1.30 m rcg legs 0.548 + 0.601+ 0.374 + 0.227 m 1.75 m With these distances and the given masses we find xcg 62.8 kg m 1.01 m 62.05 kg With the body positioned as shown in Figure P8.15c, we use the following sketch to determine the distance x for each body part: xarms rcg arms xtorso rcg arms 0.239 m torso 0.548 m 0.337 m 0.211 m Page 8.8 Chapter 8 xthighs xlegs arms arms torso torso rcg thighs thighs 0.548 0.601 0.151 m 0.204 m rcg legs 0.548 0.601 0.374 0.227 m 0.654 m With these distances, the location (relative to the bar) of the center of gravity of the body is xcg 8.16 0.924 kg m 0.015 m 0.015 m towards the head 62.05 kg With the coordinate system shown below, the coordinates of the center of gravity of each body part may be computed: xcg,arms 0 ycg,arms xcg,torso rcg xcg,thighs xcg,legs torso torso torso arms rcg arms 0.309 m 0.337 m ycg,torso 0 thighs ycg,thighs rcg thighs thighs cos 60.0 rcg ycg,legs thighs sin 60.0 0.324 m rcg cos 60.0 0.676 m legs 1.02 m sin 60.0 0.131 m With these coordinates for individual body parts and the masses given in Problem 8.15, the coordinates of the center of mass for the entire body are found to be xcg marms xcg,arms mtorso xcg,torso mthighs xcg,thighs mlegs xcg,legs marms mtorso mthighs mlegs and Page 8.9 28.5 kg m 0.459 m 62.05 kg Chapter 8 ycg 8.17 marms ycg,arms mtorso ycg,torso mthighs ycg,thighs mlegs ycg,legs marms mtorso mthighs mlegs 6.41 kg m 0.103 m 62.05 kg The free-body diagram for the spine is shown below. When the spine is in rotational equilibrium, the sum of the torques about the left end (point O) must be zero. Thus, 2L L Ty 350 N 200 N L 0 3 2 Yielding Ty T sin12.0 562 N . The tension in the back muscle is then T 562 N = 2.71 103 N 2.71 kN . sin 12.0 The spine is also in translational equilibrium, so Fx 0 Rx Tx 0 and the compression force in the spine is Rx Tx T cos12.0= 2.71 kN cos12.0 2.65 kN 8.18 In the free-body diagram of the foot given at the right, note that the force R (exerted on the foot by the tibia) has been replaced by its horizontal and vertical components. Employing both conditions of equilibrium (using point O as the pivot point) gives the following three equations: Page 8.10 Chapter 8 Fx 0 R sin15.0 T sin 0 or R T sin sin 15.0 [1] Fy 0 700 N R cos15.0 T cos 0 [2] 700 N 18.0 cm cos T 25.0 cm 18.0 cm 0 O 0 or T = (1 800 N) cos [3] Substituting Equation [3] into Equation [1] gives 1 800 N R sin cos sin 15.0 [4] Substituting Equations [3] and [4] into Equation [2] yields 1 800 N 2 tan 15.0 sin cos 1 800 N cos 700 N which reduces to: sin cos = (tan 15.0º) cos2 + 0.104 2. Squaring this result and using the identity sin2 1 cos2 gives tan2 15.0 1 cos4 2 tan 15.0 0.104 2 1 cos2 0.104 2 0 2 In this last result, let u = cos2 and evaluate the constants to obtain the quadratic equation 1.071 8 u2 0.944 2 u 0.010 9 0 The quadratic formula yields the solutions u = 0.869 3 and u = 1.011 7. Thus, cos1 0.869 3 21.2 or cos1 0.011 7 83.8 Page 8.11 Chapter 8 We ignore the second solution since it is physically impossible for the human foot to stand with the sole inclined at 83.8° to the floor. We are the left with: = 21.2º. Equation [3] then yields T 1 800 N cos 21.2 1.68 103 N and Equation [1] gives R 8.19 1.68 103 N sin 21.2 sin 15.0 2.34 103 N Consider the torques about an axis perpendicular to the page through the left end of the rod. 0 T 100 N 3.00 m 500 N 4.00 m 6.00 m cos 30.0 T 443 N Fx 0 Rx T sin 30.0 443 N sin 30.0 Rx = 221 N toward the right Fy 0 Ry T cos 30.0 100 N 500 N 0 Ry = 600 N (443 N) cos 30.0 = 217 N upward 8.20 Consider the torques about an axis perpendicular to the page through the left end of the scaffold. 0 T1 0 700 N 1.00 m 200 N 1.50 m T2 3.00 m 0 From which, T2 = 333 N. Page 8.12 Chapter 8 Then, from Fy = 0, we have T1+T2 – 700 N – 200 N = 0 or T1 = 900 N – T2 = 900 N – 333 N = 567 N 8.21 Consider the torques about an axis perpendicular to the page and through the left end of the plank. = 0 gives 700 N 0.500 m 294 N 1.00 m T1 sin 40.0 2 .00 m 0 or T1 = 501 N. Then, Fx 0 gives T3 T1 cos 40.0° 0 , or T3 501 N cos 40.0 384 N From Fy 0 , T2 994 N T1 sin 40.0 0 , or T2 994 N 501 N sin 40.0 672 N . 8.22 (a) See the diagram below (b) If x = 1.00 m, then left end 0 700 N 1.00 m 200 N 3.00 m 80.0 N 6.00 m T sin 60.0° 6.00 m 0 Page 8.13 Chapter 8 giving T = 434 N. Then, Fx 0 H T cos 60.0° 0 , or H 343 N cos 60.0° 172 N and Fy 0 V 980 N + 343 N sin 60.0° 0 , or V = 683 N. (c) When the wire is on the verge of breaking, T = 900 N and left end 700 N xmax 200 N 3.00 m 80.0 N 6.00 m 900 N sin 60.0° 6.00 m 0 which gives xmax = 5.14 m 8.23 The required dimensions are as follows: d1 4.00 m cos 50.0° 2 .57 m d2 d cos 50.0° 0.643 d d3 8.00 m sin 50.0 6.13 m Fy 0 yields F1 200 N 800 N = 0 , or F1 = 1.00 103 N. When the ladder is on the verge of slipping, f fs max s n s F1 or f 0.600 1.00 103 N 600 N Then, Fx = 0 gives F2 = 600 N to the left. Finally, using an axis perpendicular to the page and through the lower end of the ladder = 0, gives –(200 N)(2.57 m) – (800 N)(0.643)d+(600 N)(6.13 m) = 0 or d 3.68 103 550 0.643 800 N Nm 6.15 m when the ladder is ready to slip Page 8.14 Chapter 8 8.24 (a) (b) The point of intersection of two unknown forces is always a good choice as the pivot point in a torque calculation. Doing this eliminates these two unknowns from the calculation (since they have zero lever arms about the chosen pivot) and makes it .easier to solve the resulting equilibrium equation . L 0 0 mg cos T L sin 0 2 (c) hinge 0 (d) Solving the above result for the tension in the cable gives T mg 2 L cos L sin mg 2 tan or T 16.0 kg 9.80 m s2 2 tan 30.0 136 N Fy mg 0 (f) Solving the above results for the components of the hinge force gives (g) and and Fy mg 16.0 kg 9.80 m s2 157 N Attaching the cable higher up would allow the cable to bear some of the weight, thereby reducing the stress on the hinge. It would also reduce the tension in the cable. 8.25 Fx 0 Fx = T = 136 N Fx T 0 Fy 0 (e) Consider the free-body diagram of the material making up the center point in Page 8.15 Chapter 8 the rope given at the right. Since this material is in equilibrium, it is necessary to have Fx = 0 and Fy = 0, giving Fx 0: T2 sin T1 sin 0 or T2 = T1, meaning that the rope has a uniform tension T throughout its length. T cos T cos 475 N 0 where cos Fy 0: 0.500 m 6.00 m 2 0.500 m 2 and the tension in the rope (force applied to the car) is 475 N 475 N T 2 cos 8.26 6.00 m 2 0.500 m 2 2 0.500 m 2.86 103 N 2.86 kN (a) (b) lower 0 or T (c) Fx 0 Fy 0 end L 0 0 mg cos T L sin 0 2 mg cos mg cot 2 sin 2 T s n 0 n mg 0 or T s n [1] n mg [2] Substitute Equation [2] into [1] to obtain T = smg. Page 8.16 Chapter 8 (d) Equate the results of parts (b) and (c) to obtain s = cot /2 This result is valid only at the critical angle where the beam is on the verge of slipping (i.e., where fs = (fs)max is valid.) (e) At angles below the critical angle (where fs fs max is valid), the beam will slip. At larger angles, the static friction force is reduced below the maximum value, and it is no longer appropriate to use s in the calculation. 8.27 Consider the torques about an axis perpendicular to the page and through the point where the force T acts on the jawbone. 0 (50.0 N) (7.50 cm) R (3.50 cm) 0 , which yields R 107 N . Then, Fy 0 50.0 N + T 107 N 0 , or T 157 N . 8.28 Observe that the cable is perpendicular to the boom. Then, using = 0 for an axis perpendicular to the page and through the lower end of the boom gives L 3 1.20 kN cos 65° T 2 4 L 2.00 kN L cos 65° 0 or .T = 1.47 kN From Fx 0 , H T cos 25° 1.33 kN to the right and Fy = 0 gives V = 3.20 kN – T sin 25 = 2.58 kN upward 8.29 First, we resolve all forces into components parallel to and perpendicular to the tibia, as shown. Note that = 40.0 and Page 8.17 Chapter 8 wy = (30.0 N) sin 40.0 = 19.3 N Fy = (12.5 N) sin 40.0 = 8.03 N and Ty = T sin 25.0 Using = 0 for an axis perpendicular to the page and through the upper end of the tibia gives d d T sin 25.0° 5 19.3 N 2 8.03 N d 0 or T = 209 N. 8.30 When x = xmin , the rod is on the verge of slipping, so f fs max s n 0.50 n From Fx 0 , n T cos 37° 0, or n 0.80 T . Thus, f 0.50 0.80 T 0.40 T From Fy 0 , f T sin 37 2 w 0, or 0.40 T 0.60 T 2 w 0 , giving T 2 w Using = 0 for an axis perpendicular to the page and through the left end of the beam gives w xmin w 2.0 m 2 w sin 37° 4.0 m 0 , which reduces to xmin = 2.8 m. 8.31 The moment of inertia for rotations about an axis is I mi ri2 , where ri is the distance mass mi is from that axis. (a) For rotation about the x-axis, I x 3.00 kg 3.00 m 2 .00 kg 3.00 m 2 2 2.00 kg 3.00 m 4.00 kg 3.00 m 99.0 kg m 2 2 2 Page 8.18 Chapter 8 (b) When rotating about the y-axis, I y 3.00 kg 2 .00 m 2 .00 kg 2 .00 m 2 2 2.00 kg 2.00 m 4.00 kg 2.00 m 44.0 kg m 2 2 (c) 2 For rotations about an axis perpendicular to the page through point O, the distance ri for each mass is ri 2 .00 m 2 3.00 m 2 13.0 m Thus, IO 3.00 2.00 2.00 4.00 kg 13.0 m2 143 kg m2 8.32 The required torque in each case is = I. Thus, x Ix 99.0 kg m2 1.50 rad s2 149 N m y I y 44.0 kg m2 1.50 rad s2 66.0 N m and O IO 143 kg m2 1.50 rad s2 215 N m 8.33 net 0.330 m 250 N 87.8 kg m 2 rF sin 90 0.940 rad s2 (a) net I (b) For a solid cylinder, I = Mr2/2, so M (c) I 2 87.8 kg m2 2I r2 0.330 m 2 1.61 103 kg 0 t 0 0.940 rad s2 5.00 s 4.70 rad s Page 8.19 Chapter 8 8.34 (a) I 2Idisk Icylinder 2 MR2 2 mr 2 2 or I MR2 mr 2 2 (b) g = 0 Since the line of action of the gravitational force passes through the rotation axis, it has zero lever arm about this axis and zero torque. (c) The torque due to the tension force is positive. Imagine gripping the cylinder with your right hand so your fingers on the front side of the cylinder point upward in the direction of the tension force. The thumb of your right hand then points toward the left (positive direction) along the rotation axis. Because I , the torque and angular acceleration have the same direction. Thus, a positive torque produces a positive angular acceleration. When released, the center of mass of the yoyo drops downward, in the negative direction. The translational acceleration is negative. (d) Since, with the chosen sign convention, the translational acceleration is negative when the angular acceleration is positive, we must include a negative sign in the proportionality between these two quantities. Thus, we write: a = r or = –a/r (e) Translation: Fy mtotal a (f) T 2M m g 2M m a [1] Rotational: I (g) rT sin 90 I or rT I [2] Substitute the results of (d) and (a) into Equation [2] to obtain mr 2 a a r T I I MR 2 r r 2 r 2 R2 m T M as 2 r or Substituting Equation [3] into [1] yields 2 M R r m 2 a 2 M m g 2 M m a Page 8.20 or a 2M m g 2 M M R r 3m 2 2 [3] Chapter 8 8.35 2 2.00 kg 1.00 kg 9.80 m s2 (h) a (i) From Equation [1], T 2M m g a 5.00 kg 9.80 m s2 2.72 m s2 35.4 N . ( j) y 0 t at 2 2 (a) Consider the free-body diagrams of the cylinder and 2 2.00 kg 2.00 kg 10.0 4.00 3 1.00 kg 2 2 2.72 m s2 2 y t a 2 1.00 m 2.72 m s2 0.857 s man given at the right. Note that we shall adopt a sign convention with clockwise and downward as the positive directions. Thus, both a and are positive in the indicated directions and a = r. We apply the appropriate form of Newton’s second law to each diagram to obtain the following: Rotation of Cylinder: I rT sin 90° I , or T I r, so T 11 a Mr 2 r r 2 and 1 Ma 2 T [1] Translation of man: Fy ma mg T ma Equating Equations [1] and [2] gives a (b) T m g a or 1 2 Ma m g a , or 75.0 kg 9.80 m s2 mg 3.92 m s2 m M 2 75.0 kg+ 225 kg 2 From a = r, we have Page 8.21 [2] Chapter 8 a 3.92 m s2 9.80 rad s2 r 0.400 m (c) As the rope leaves the cylinder, the mass of the cylinder decreases, thereby decreasing the moment of inertia. At the same time, the weight of the rope leaving the cylinder would increase the downward force acting tangential to the cylinder, and hence increase the torque exerted on the cylinder. Both of these effects will cause the acceleration of the system to increase with time. (The increase would be slight in this case, given the large mass of the cylinder.) 8.36 The angular acceleration is ( f i ) t (i t ) since f 0 Thus, the torque is I (I i t ) . But, the torque is also = – fr, so the magnitude of the required friction force is f 12 kg m 2 50 rev min 2 rad 1 min I i 1 rev 60 s 21 N r t 0.50 m 6.0 s Therefore, the coefficient of friction is k 8.37 8.38 f 21 N 0.30 n 70 N (a) F r 0.800 N 30.0 m 24.0 N m (b) (c) a t r 30.0 m 0.0356 rad s2 1.07 m s2 I m r2 24.0 N m 0.750 kg 30.0 m 2 0.0356 rad s2 I MR2 1.80 kg 0.320 m 0.184 kg m2 2 net applied resistive I , or F r f R I yielding Page 8.22 Chapter 8 F 8.39 (a) F (b) F I I f R r 0.184 kg m2 4.50 rad s2 120 N 0.320 m 4.50 0.184 kg m2 4.50 10 2 m rad s2 120 N 0.320 m 2.80 10 2 m 872 N 1.40 kN 1 1 2 MR2 150 kg 1.50 m 169 kg m 2 2 2 and f i t 0.500 rev s 0 2 rad 2 1 rev 2 rad s 2 .00 s Thus, F r I gives I F r 8.40 (a) 169 kg m2 2 rad s2 1.50 m 177 N It is necessary that the tensions T1 and T2 be different in order to provide a net torque about the axis of the pulley and produce and angular acceleration of the pulley. Since intuition tells us that the system will accelerate in the directions shown in the diagrams at the right when m2 > m1, it is necessary that T2 > T1. (b) We adopt a sign convention for each object with the positive direction being the indicated direction of the acceleration of that object in the diagrams at the right. Then, apply Newton’s second law to each object: For m1 : Fy m1a T1 m1g m1a or T1 m1 g a [1] For m2 : Fy m2 a m2 g T2 m2 a m2 or T2 m2 g a [2] Page 8.23 Chapter 8 I For M : rT2 rT1 I T2 T1 I r or [3] Substitute Equations [1] and [2], along with the relations I Mr 2 2 and a r , into Equation [3] to obtain m2 g a m1 g a Mr 2 a Ma 2r r 2 M m1 m2 2 a m2 m1 g or and a (c) m2 m1 g m1 m2 M 2 20.0 kg 10.0 kg 9.80 m s2 20.0 kg 10.0 kg + 8.00 kg 2 2.88 m s2 From Equation [1]: T1 10.0 kg 9.80 m s2 2.88 m s2 127 N . From Equation [2]: T2 20.0 kg 9.80 m s2 2.88 m s2 138 N . 8.41 The initial angular velocity of the wheel is zero, and the final angular velocity is f v 50.0 m s 40.0 rad s r 1.25 m Hence, the angular acceleration is f i t 40.0 rad s 0 83.3 rad s2 0.480 s The torque acting on the wheel is fk r , so I gives fk 110 kg m 2 83.3 rad s2 I r 1.25 m 7.33 103 N Thus, the coefficient of friction is k fk 7.33 103 N 0.524 n 1.40 10 4 N Page 8.24 Chapter 8 8.42 (a) The moment of inertia of the flywheel is I 1 1 2 MR2 500 kg 2 .00 m 1.00 103 kg m 2 2 2 and the angular velocity is rev 2 rad 1 min 5000 524 rad s min 1 rev 60 s Therefore, the stored kinetic energy is 1 1 I2 1.00 103 kg m 2 2 2 KEstored (b) 524 rad s 1.37 108 J 2 A 10.0-hp motor supplies energy at the rate of 746 W 7.46 103 J s 1 hp P 10.0 hp The time the flywheel could supply energy at this rate is t 8.43 KEstored P 1.37 108 J 1.84 10 4 s 5.10 h 7.46 103 J s The moment of inertia of the cylinder is I 1 1 w 1 800 N 2 MR 2 R 2 1.50 m 91.8 kg m 2 2 2 2 g 2 9.80 m s The angular acceleration is given by I 50.0 N 1.50 m 0.817 rad s2 FR I 91.8 kg m 2 At t = 3.00 s, the angular velocity is Page 8.25 Chapter 8 i t 0 0.817 rad s2 3.00 s 2 .45 rad s and the kinetic energy is KErot 8.44 (a) (b) 1 1 I2 91.8 kg m2 2 2 2.45 rad s 276 J 2 Hoop: I MR2 4.80 kg 0.230 m 0.254 kg m 2 Solid Cylinder: I 1 1 2 MR2 4.80 kg 0.230 m 0.127 kg m 2 2 2 Solid Sphere: I 2 2 2 MR2 4.80 kg 0.230 m 0.102 kg m 2 5 5 Thin, Spherical, Shell: I 2 2 2 MR2 4.80 kg 0.230 m 0.169 kg m 2 3 3 2 When different objects of mass M and radius R roll without slipping a R down a ramp, the one with the largest translational acceleration a will have the highest translational speed at the bottom. To determine the translational acceleration for the various objects, consider the free-body diagram at the right: Fx Ma I Mg sin f Ma f R I a R [1] or f Ia R2 [2] Substitute Equation [2] into [1] to obtain Mg sin Ia R2 Ma or a Mg sin M I R2 Since M, R, g are the same for all of the objects, we see that the translational acceleration (and hence the translational speed) increases as the moment of inertia decreases. Thus, the proper rankings from highest to lowest by translational speed will be: Page 8.26 Chapter 8 Solid sphere; solid cylinder; thin, spherical, shell; and hoop (c) When an object rolls down the ramp without slipping, the friction force does no work and mechanical energy is conserved. Then, the total kinetic energy gained equals the gravitational potential energy given up: KEr KEt PEg Mgh and KEr Mgh 1 2 Mv2 , where h is the vertical drop of the ramp and is the translational speed at the bottom. Since M, g, and h are the same for all of the objects, the rotational kinetic energy decreases as the translational speed increases. Using this fact, along with the result of Part (b), we rank the object’s final rotational kinetic energies, from highest to lowest, as: hoop; thin, spherical, shell; solid cylinder; and solid sphere 8.45 (a) Treating the particles on the ends of the rod as point masses, the total moment of inertia of the rotating system is I Irod I3 I 4 mrod L2 12 m3 (L 2)2 m4 (L 2)2 . If the mass of the rod can be ignored, this reduces to L I 0 m3 m4 2 2 3.00 kg 4.00 kg 0.500 m 1.75 kg m 2 2 and the rotational kinetic energy is KEr (b) 1 1 I2 1.75 kg m 2 2 2 2.50 rad s 5.47 J 2 If the rod has mass mrod 2.00 kg I 1 2 2.00 kg 1.00 m 1.75 kg m 2 1.92 kg m 2 12 and KEr 8.46 1 1 I2 1.92 kg m 2 2 2 2.50 rad s 6.00 J 2 Using conservation of mechanical energy, KE trans KErot PEg f KEtrans KErot PEg or Page 8.27 i Chapter 8 1 1 M vt2 I 2 0 0 0 M g L sin 2 2 Since I 2 5 MR2 for a solid sphere and vt R when rolling without slipping, this becomes 1 1 M R2 2 M R 2 2 M g L sin 2 5 and reduces to 8.47 (a) 10 gL sin 7 R2 10 9.8 m s2 6.0 m sin 37 7 0.20 m 2 36 rad s Assuming the disk rolls without slipping, the friction force between the disk and the ramp does no work. In this case, the total mechanical energy of the disk is constant with the value E KEi (PEg )i 0 Mgh MgL sin . When the disk gets to the bottom of the ramp, PEg 0 and KE f KEt KEr E MgL sin . Also, since the disk does not slip, v R and KEr 1 1 I2 2 2 1 2 v 2 MR R 2 1 2 1 1 2 2 M v 2 KEt Then, KEtotal KEt 1 KEt E MgL sin or 2 31 M v2 M gL sin 2 2 and v (b) 4 gL sin 3 4 9.80 m s2 4.50 m sin 15.0 3 The angular speed of the disk at the bottom is v 3.90 m s 15.6 rad s R 0.250 m Page 8.28 3.90 m s Chapter 8 8.48 (a) Assuming the solid sphere starts from rest, and taking y =0 at the level of the bottom of the incline, the total mechanical energy will be split among three distinct forms of energy E PEg i mgh as the sphere rolls down the incline. These are rotational kinetic energy, 1 I2 2 translational kinetic energy, 1 mv2 2 and gravitational potential energy, mgy where y is the current height of the center of mass of the sphere above the level of the bottom of the incline. (b) The force of static friction, exerted on the sphere by the incline and directed up the incline, exerts a torque about the center of mass giving the sphere an angular acceleration. (c) KEt I 2 5 1 2 Mv2 and KEr 1 2 I 2 where v R (since the sphere rolls without slipping) and MR2 for a solid sphere. Therefore, 2 MR2 5 2 KEr I2 2 2 MR2 2 2 2 2 2 KEt KEr Mv 2 I 2 7 5 MR2 2 2 MR2 2 M R 2 MR2 5 2 8.49 Using Wnet KE f KEi f 8.50 1 2 I 2f 0 , we have 2F s I 2 Wnet I 2 5.57 N 0.800 m 4.00 10 4 kg m 2 149 rad s The work done on the grindstone is Wnet F s F r F r . Thus, Wnet 1 2 I 2f 1 2 I i2 , or Page 8.29 Chapter 8 25.0 N m 15.0 rev 2 rad 1 0.130 kg m 2 2f 0 1 rev 2 This yields rad 1 rev 30.3 rev s s 2 rad f 190 8.51 (a) KEtrans KErot (b) (c) 8.52 1 1 2 mvt2 10.0 kg 10.0 m s 500 J 2 2 1 2 1 1 v2 I mR 2 t2 R 2 2 2 1 1 2 mvt2 10.0 kg 10.0 m s 250 J 4 4 KEtotal KEtrans KErot 750 J As the bucket drops, it loses gravitational potential energy. The spool gains rotational kinetic energy and the bucket gains translational kinetic energy. Since the string does not slip on the spool, r where r is the radius of the spool. The moment of inertia of the spool is I 1 2 where M is the mass of the spool. Conservation of energy gives KE t KEr PEg f KEt KEr PEg i 1 1 m 2 I 2 mgy f 0 0 mgyi 2 2 or 1 11 2 m r Mr 2 2 mg yi y f 2 22 Page 8.30 Mr 2 , Chapter 8 This gives 8.53 (a) 2mg yi y f m 1 2 M r2 2 3.00 kg 9.80 m s2 3.00 kg+ 1 2 4.00 m 5.00 kg 0.600 m 2 10.9 rad s The arm consists of a uniform rod of 10.0 m length and the mass of the seats at the lower end is negligible. The center of gravity of this system is then located at the geometric center of the arm, located 5.00 m from the upper end. From the sketch at the right, the height of the center of gravity above the zero level is ycg 10.0 m 5.00 m cos . (b) When 45.0 , ycg 10.0 m 5.00 m cos 45.0 6.46 m and PEg mgycg 365 kg 9.80 m s2 (c) 6.46 m 2.31 104 J In the vertical orientation, = 0 and cos = 1, giving ycg 10.0 m 5.00 m 5.00 m . Then, PEg mgycg 365 kg 9.80 m s2 (d) 5.00 m 1.79 104 J Using conservation of mechanical energy as the arm starts from rest in the 45° orientation and rotates about the upper end to the vertical orientation gives 1 I end 2f mg ycg 2 f 0 mg ycg i or f For a long, thin rod: Iend mL2 3 . Equation [1] then becomes Page 8.31 2mg ycg ycg i I end f [1] Chapter 8 2 m g ycg ycg i m L2 3 f 6 9.80 m s2 f y 6 g ycg i cg f L2 6.46 m 5.00 m 10.0 m 2 0.927 rad s Then, from r , the translational speed of the seats at the lower end of the rod is 10.0 m 0.927 rad s 9.27 m s 8.54 8.55 (a) L I MR2 2.40 kg 0.180 m (b) 1 1 2 L I MR 2 2.40 kg 0.180 m 35.0 rad s 1.36 kg m 2 s 2 2 (c) 2 2 2 L I MR 2 2.40 kg 0.180 m 35.0 rad s 1.09 kg m 2 s 5 5 (d) 2 2 2 L I MR 2 2.40 kg 0.180 m 35.0 rad s 1.81 kg m 2 s 3 3 (a) The rotational speed of Earth is E 2 35.0 rad s 2.72 kg m 2 s 2 rad 1d 7.27 10 5 rad s 1 d 8.64 10 4 s 2 Lspin I sphere E M E RE2 E 5 2 5.98 10 24 kg 6.38 10 6 m 5 Page 8.32 2 7.27 10 5 rad s 7.08 10 33 J s Chapter 8 (b) For Earth’s orbital motion, orbit 2 rad 1y 1y 3.156 107 1.99 10 7 rad s s and using data from Table 7.3, we find 2 Lorbit I point orbit ME Rorbit orbit 5.98 1024 kg 1.496 1011 m 8.56 (a) 2 1.99 107 rad s 2.67 10 40 J s Yes, the bullet has angular momentum about an axis through the hinges of the door before the collision. Consider the sketch at the right, showing the bullet the instant before it hits the door. The physical situation is identical to that of a point mass mg moving in a circular path of radius r with tangential speed t = i. For that situation the angular momentum is Li I i i mB r 2 i mB r i r and this is also the angular momentum of the bullet about the axis through the hinge at the instant just before impact. (b) No, mechanical energy is not conserved in the collision. The bullet embeds itself in the door with the two moving as a unit after impact. This is a perfectly inelastic collision in which a significant amount of mechanic cal energy is converted to other forms, notably thermal energy. (c) Apply conservation of angular momentum with Li mBri as discussed in part (a). After impact, L f I f f I door I bullet f 1 2 Mdoor L2 mBr 2 f where L = 1.00 m = the width of the door and r = L – 10.0 cm = 0.900 m. Then, L f Li f mB ri 1 Mdoor L2 mB r 2 3 0.005 kg 0.900 m 1.00 103 ms 1 2 2 18.0 kg 1.00 m 0.005 kg 0.900 m 3 Page 8.33 Chapter 8 yielding f 0.749 rad s . (d) The kinetic energy of the door-bullet system immediately after impact is 1 1 1 2 2 2 I f 2f 18.0 kg 1.00 m 0.005 kg 0.900 m 0.749 rad s 2 2 3 KE f or KE f 1.68 J . The kinetic energy (of the bullet) just before impact was KEi 8.57 1 1 mBi2 0.005 kg 1.00 103 m s 2 2 2 2.50 103 J Each mass moves in a circular path of radius r = 0.500 m/s about the center of the connecting rod. Their angular speed is r 5.00 m s 10.0 m s 0.500 m Neglecting the moment of inertia of the light connecting rod, the angular momentum of this rotating system is L I m1r 2 m2r 2 4.00 kg 3.00 kg 0.500 m 10.0 rad s 17.5 J s 2 8.58 Using conservation of angular momentum, Laphelion Lperihelion . Thus, mra2 a mrp2 p . Since = 1/r at both aphelion and perihelion, this is equivalent to mra2 a ra mrp2 p rp , giving rp 0.59 A.U. a p 54 km s 0.91 km s 35 A.U. ra 8.59 The initial moment of inertia of the system is 2 Ii mi ri2 4 M 1.0 m M 4.0 m 2 Page 8.34 Chapter 8 The moment of inertia of the system after the spokes are shortened is 2 I f m f rf2 4 M 0.50 m M 1.0 m 2 From conservation of angular momentum, If f = Ii i, or Ii i 4 2.0 rev s 8.0 rev s If f 8.60 From conservation of angular momentum: I child I m-g -r f f Ichild I m -g -r i i where I m-g-r 275 kg m2 is the constant moment of inertia of the merry-go-round. Treating the child as a point object, Ichild mr 2 where r is the distance the child is from the rotation axis. Conservation of angular momentum then gives f 25.0 kg 1.00 m 2 275 kg m 2 mri2 I m-g-r 14.0 rev min 2 i 25.0 kg 2.00 m 2 275 kg m 2 mrf I m-g-r or f 11.2 8.61 rev 2 rad min 1 rev 1 min 60.0 s 1.17 rad s The moment of inertia of the cylinder before the putty arrives is Ii 1 1 2 M R2 10.0 kg 1.00 m 5.00 kg m 2 2 2 After the putty sticks to the cylinder, the moment of inertia is I f Ii mr 2 5.00 kg m2 0.250 kg 0.900 m 5.20 kg m2 2 Conservation of angular momentum gives If f = Ii i, or Page 8.35 Chapter 8 Ii 5.00 kg m2 7.00 rad s 6.73 rad s i 5.20 kg m2 If f 8.62 The total moment of inertia of the system is Itotal I masses I student 2 mr 2 3.0 kg m2 2 Initially, r = 1.0 m, and Ii 2 3.0 kg 1.0 m 3.0 kg m 2 9.0 kg m 2 . Afterward, r = 0.30 m, so 2 I f 2 3.0 kg 0.30 m 3.0 kg m 2 3.5 kg m 2 (a) From conservation of angular momentum, If f = Ii i, or Ii 9.0 kg m2 0.75 rad s 1.9 rad s i 3.5 kg m2 If f (b) 8.63 KEi 1 1 2 Ii i2 9.0 kg m 2 0.75 rad s 2.5 J 2 2 KE f 1 1 2 I f 2f 3.5 kg m 2 1.9 rad s 6.3 J 2 2 The initial angular velocity of the puck is i t i ri 0.800 m s rad 2 .00 0.400 m s Since the tension in the string does not exert a torque about the axis of revolution, the angular momentum of the puck is conserved, or If f = Ii i. Thus, f 2 Ii mri2 0.400 m i 2 i 2 .00 rad s 5.12 rad s 0.250 m If mrf Page 8.36 Chapter 8 The net work done on the puck is Wnet KE f KEi 1 1 1 m 2 2 rf f ri2i2 I f 2f I i i2 mrf2 2f mri2 i2 2 2 2 2 or 0.120 kg Wnet 2 0.250 m 5.12 rad s 0.400 m 2 2 2 2 .00 2 rad s This yields Wnet 5.99 102 J . 8.64 For one of the crew, Fc m ac becomes n m vt2 /r mr i2 . We require n = mg, so the initial angular velocity must be i g/r . From conservation of angular momentum, I f f Ii i or f (Ii /I f )i . Thus, the angular velocity of the station during the union meeting is f I i If 5.00 108 kg m 2 150 65.0 kg 100 m 2 g g g 1.12 2 r r 5.00 108 kg m 2 50 65.0 kg 100 m r The centripetal acceleration experienced by the managers still on the rim is ac r 2f r 12.3 m s2 1.12 8.65 (a) 2 g 2 1.12 9.80 m s2 12.3 m s2 r From conservation of angular momentum, If f = Ii i, so Ii If f I1 o i I1 I 2 2 (b) I I 1 1 1 I KE f I f 2f I1 I 2 1 o2 1 I1 o2 1 KEi 2 2 I1 I2 I1 I2 2 I1 I2 or Page 8.37 Chapter 8 KE f KEi I1 I1 I 2 Since this is less than 1.0, kinetic energy was lost. 8.66 The initial angular velocity of the system is rev 2 rad 0.40 rad s s 1 rev i 0.20 The total moment of inertia is given by I I man I cylinder mr 2 1 1 2 M R2 80 kg r 2 25 kg 2 .0 m 2 2 Initially, the man is at r 2.0 m from the axis, and this gives Ii 3.7 102 kg m2 . At the end, when r = 1.0, the moment of inertia is I f 1.3 102 kg m2 . (a) From conservation of angular momentum, If f = Ii i, or Ii 3.7 102 kg m2 0.40 rad s 1.14 rad s 3.6 rad s i 1.3 102 kg m2 If f (b) The change in kinetic energy is KE KE 1 I 2 f 2f 21 I f i2 , or 2 1 rad 1 rad 1.3 102 kg m 2 1.14 3.7 10 2 kg m 2 0.40 2 s 2 s 2 or KE 5.4 102 J . The difference is the work done by the man as he walks inward. 8.67 (a) The table turns counterclockwise, opposite to the way the woman walks. Its angular momentum cancels that of the woman so the total angular momentum maintains a constant value of Ltotal Lwoman Ltable 0 . Since the final angular momentum is Ltotal Iw w It t 0 , we have Page 8.38 Chapter 8 I mw r 2 I t w w It t mw r w r I w t or 60.0 kg 2 .00 m 1.50 m s 0.360 rad s 500 kg m 2 t Hence, table 0.360 rad s counterclockwise . (b) Wnet KE KE f 0 Wnet 8.68 (a) 1 1 mw2 I t t2 2 2 1 1 2 2 60.0 kg 1.50 m s 500 kg m 2 0.360 rad s 99.9 J 2 2 In the sketch at the right, choose an axis perpendicular to the page and passing through the indicated pivot. Then, with = 30.0, the lever arm of the force P is observed to be 5.00 cm 5.00 cm 5.77 cm cos cos 30.0 and = 0 gives P 5.77 cm 150 N 30.0 cm 0 so P (b) 150 N 30.0 cm 5.77 cm 780 N Fy 0 n P cos 30.0 0 , giving n P cos 30.0 780 N cos30.0 675 N Page 8.39 Chapter 8 Fx 0 f F P sin 30.0 0 , or f P sin 30.0 F 780 N sin 30.0 150 N 240 N The resultant force exerted on the hammer at the pivot is R f 2 n2 240 N 2 675 N 2 716 N at tan1 (n/f ) tan1(675 N/240 N) 70.4 , or R 716 N at 70.4 above the horizontal to the right 8.69 (a) Since no horizontal force acts on the child-boat system, the center of gravity of this system will remain stationary, or xcg mchild xchild mboat xboat constant mchild mboat The masses do not change, so this result becomes mchild xchild + mboatxboat = constant. Thus, as the child walks to the right, the boat will move to the left . (b) Measuring distances from the stationary pier, with away from the pier being positive, the child is initially at (xchild)i = 3.00 m and the center of gravity of the boat is at (xboat)i = 5.00. At the end, the child is at the right end of the boat, so (xchild)f = (xboat)f + 2.00 m. Since the center of gravity of the system does not move, we have mchild xchild mboat xboat f mchild xchild mboat xboat i , or mchild xchild f mboat xchild f 2.00 m mchild 3.00 m mboat 5.00 m and xchild f xchild f mchild 3.00 m mboat 5.00 m 2.00 m mchild mboat 40.0 kg 3.00 m 70.0 kg 5.00 m 2.00 m 40.0 kg 70.0 kg Page 8.40 5.55 m Chapter 8 (c) When the child arrives at the right end of the boat, the greatest distance from the pier that he can reach is xmax xchild f 1.00 m 5.55 m 1.00 m 6.55 m This leaves him 0.45 m short of reaching the turtle . 8.70 (a) Consider the free-body diagram of the block given at the right. If the +x-axis is directed down the incline, Fx = max gives mg sin 37.0 T m at , or T m g sin 37.0 at T 12.0 kg 9.80 m s2 sin 37.0 2.00 m s 2 46.8 N (b) Now, consider the free-body diagram of the pulley. Choose an axis perpendicular to the page and passing through the center of the pulley, = I gives at T r I r or I (c) 8.71 46.8 N 0.100 m T r2 at 2.00 m s2 a 2 0.234 kg m2 2.00 m s2 i t 0 t t 2.00 s 40.0 rad s r 0.100 m If the ladder is on the verge of slipping, f fs max s n at both the floor and the wall. From Fx = 0, we find f1 – n2 = 0, or n2 = sn1 [1] Also, Fx = 0 gives n1 – w + sn2.= 0 Page 8.41 Chapter 8 Using Equation [1], this becomes n 1 w s s n1 0 or n 1 w w 0.800 w 2 1 s 1.25 [2] Thus, Equation [1] gives n2 0.500 0.800 w 0.400 w [3] Choose an axis perpendicular to the page and passing through the lower end of the ladder. Then, = 0 yields L w cos n2 L sin f2 L cos 0 2 Making the substitutions n2 = 0.400 w and f2 s n2 0.200 w , this becomes L w cos 0.400 w L sin 0.200 w L cos 0 2 and reduces to 0.500 0.200 sin cos 0.400 Hence, tan = 0.750 and = 36.9 . 8.72 Page 8.42 Chapter 8 We treat each astronaut as a point object, m, moving at speed v in a circle of radius r = d/2. Then the total angular momentum is L I1 I 2 2 mr 2 2mr r (a) Li 2mi ri 2 75.0 kg 5.00 m s 5.00 m Li 3.75 103 kg m2 s (b) KEi 1 1 1 m1 12i m2 22i 2 mi2 2 2 2 KEi 75.0 kg 5.00 m s 1.88 103 J= 1.88 kJ 2 8.73 (c) Angular momentum is conserved: L f Li 3.75 103 kg m2 s . (d) f (e) 1 2 KE f 2 m 2f 75.0 kg 10.0 m s 7.50 kJ 2 (f) Wnet KE f KEi 5.62 kJ (a) d Li 2 M M d 2 (b) 1 KEi 2 M i2 M 2 2 (c) L f Li M d Lf 2 mrf 3.75 103 kg m2 s 10.0 m s 2 75.0 kg 2.50 m Page 8.43 Chapter 8 8.74 Lf M d 2 2 M d 4 (d) f (e) 1 2 KE f 2 M 2f M 2 4 M 2 2 (f) Wnet KE f KEi 3M 2 2 Mrf Choose an axis that is perpendicular to the page and passing through the left end of the scaffold. Then = 0gives 750 N 1.00 m 345 N 1.50 m 500 N 2 .00 m 1000 N 2 .50 m TR 3.00 m 0 or TR 1.59 103 N= 1.59 kN Then, Fy 0 TL 750 345 500 1000 N 1.59 103 N 1.01 kN 8.75 (a) From conservation of angular momentum, L f I f f Iii Li , or Ii i If f 2 5 2 5 2 2 Ri MRi2 1.50 109 m i i 15.0 103 m 0.010 0 rev d MR2f Rf giving f 1.00 108 (b) t f rev 2 rad 1 d 7.27 103 rad s 4 d 1 rev 8.64 10 s R f f 15.0 103 m 7.27 103 rad s 1.09 108 m s (which is about one-third the Page 8.44 Chapter 8 speed of light). 8.76 (a) Taking PEg = 0 at the level of the horizontal axis passing through the center of the rod, the total energy of the rod in the vertical position is E KE PEg 0 m1g L m2 g L (b) m1 m2 gL In the rotated position of Figure P8.76b, the rod is in motion and the total energy is E KEr PEg 1 I total 2 m1gy1 m2 gy2 2 Figure P8.76 1 m1L2 m2 L2 2 m1g L sin m2 g L sin 2 or E (c) m1 m2 L2 2 2 m1 m2 gL sin In the absence of any nonconservative forces that do work on the rotating system, the total mechanical energy of the system is constant. Thus, the results of parts (a) and (b) may be equated to yield an equation that can be solved for the angular speed, , of the system as a function of angle . (d) In the vertical position, the net torque acting on the system is zero, net = 0. This is because the lines of action of both external gravitational forces (m1g and m2g)pass through the pivot and hence have zero lever arms about the rotation axis. In the rotated position, the net torque (taking clockwise as positive) is net m1g L cos m2 g L cos m1 m2 gL cos Note that the net torque is not constant as the system rotates. Thus, the angular acceleration of the rotating system, given by = net/I, will vary as a function of . Since a net torque of varying magnitude acts on the system, the angular momentum of the system will change at a nonuniform rate. (e) In the rotated position, the angular acceleration is Page 8.45 Chapter 8 8.77 net I m1 m2 gL cos m1 L2 m2 L2 m1 m2 g cos m1 m2 L Let mp be the mass of the pulley, m1 be the mass of the sliding block, and m2 be the mass of the counterweight. (a) The moment of inertia of the pulley is I 1 m p R2p and its angular velocity at any time is, = /Rp where 2 is the linear speed of the other objects. The friction force retarding the sliding block is fk k n k m1 g Choose PEg 0 at the level of the counterweight when the sliding object reaches the second photogate. Then, from the work–energy theorem, Wnc KEtrans KErot PEg fk s f KEtrans KErot PEg i 2 1 11 f m1 m2 2f m p R 2p 2 0 Rp 2 22 1 11 2 m1 m2 i2 m p R 2p i2 m2 gs Rp 2 22 or 1 2 1 2 1 m1 m2 2 m p f 2 1 2 m1 m2 2 m p i m2 gs k m1 g s This reduces to f i2 2 m2 k m1 gs 1 m1 m2 m p 2 and yields f 2 2 0.208 kg 9.80 m s2 0.700 m m 0.820 1.63 m s s 1.45 kg Page 8.46 Chapter 8 8.78 vf 1.63 m s 54.2 rad s 0.030 0 m (b) f (a) The frame and the center of each wheel moves forward at = 3.35 m/s and each wheel also turns at angular Rp speed = /R. The total kinetic energy of the bicycle is KE = KEt + KEr, or 1 1 m frame 2 mwheel 2 2 I wheel 2 2 2 2 1 1 m frame 2 mwheel 2 mwheel R 2 2 2 2 R KE This yields KE (b) 1 m frame 3 mwheel v2 2 1 2 8.44 kg 3 0.820 kg 3.35 m s 61.2 J 2 Since the block does not slip on the roller, its forward speed must equal that of point A, the uppermost point on the rim of the roller. That is, v AE where v AE is the velocity of A relative to Earth. Since the roller does not slip on the ground, the velocity of point O (the roller center) must have the same magnitude as the tangential speed of point B (the point on the roller rim in contact with the ground). That is, vOE R O . Also, note that the velocity of point A relative to the roller center has a magnitude equal to the tangential speed R, or vAO R O . From the discussion of relative velocities in Chapter 3, we know that vAE vAO vOE . Since all of these velocities are in the same direction, we may add their magnitudes getting vAE vAO vOE , or O O 2O 2R . The total kinetic energy is KE = KEt + KEr, or Page 8.47 Chapter 8 1 1 mstone 2 2 mtree 2 2 1 1 mstone mtree 2 2 4 KE This gives KE KE 8.79 2 1 2 2 2 2 I tree 2 1 mtree R 2 2 2 4R 1 3 m mtree 2 , or 2 stone 4 1 3 2 844 kg 82.0 kg 0.335 m s 50.8 J 2 4 We neglect the weight of the board and assume that the woman’s feet are directly above the point of support by the rightmost scale. Then, the free-body diagram for the situation is as shown at the right. From Fy 0 , we have Fg1 Fg2 w 0 , or w 380 N 320 N=700 N . Choose an axis perpendicular to the page and passing through point P. Then 0 gives w x Fg1 2 .00 m 0 or Fg1 2.00 m x 8.80 w 380 N 2.00 m 700 N 1.09 m Choose PEg = 0 at the level of the base of the ramp. Then, conservation of mechanical energy gives KE trans KErot PEg f KEtrans KErot PEg i 2 1 1 mi2 mR 2 i 0 R 2 2 0 0 mg s sin or s i2 gsin R2 i2 3.0 m 3.0 rad s 24 m gsin 9.80 m s2 sin 20 2 2 Page 8.48 Chapter 8 8.81 Choose an axis perpendicular to the page and passing through the center of the cylinder. Then, applying = I to the cylinder gives 2T R 1 1 a 1 M R 2 M R 2 t or T M at 2 2 R 4 [1] Now Fy = may apply to the falling objects to obtain 2m g 2 T (a) 2m at or at g Mg M T 4 4 m which reduces to T (a) M mg M 4m From Equation [2] above, at g 8.82 [2] Substituting Equation [2] into [1] yields T (b) T m 1 M mg Mg g m M 4m M 4m 4 mg M 4m A smooth (that is, frictionless) wall cannot exert a force parallel to its surface. Thus, the only force the vertical wall can exert on the upper end of the ladder is a horizontal normal force. (b) Consider the free-body diagram of the ladder given at the right. If the rotation axis is perpendicular to the page and passing through the lower end of the ladder, the lever arm of the normal force n 2 that the wall exerts on the upper end of the ladder is d2 = L sin Page 8.49 Chapter 8 (c) The lever arm of the force of gravity, m g , acting on the ladder is d L 2 cos (d) L cos 2 Refer to the free-body diagram given in part (b) of this solution and make use of the fact that the ladder is in both translational and rotational equilibrium. Fy 0 n1 m g mp g 0 or n1 m mp g When the ladder is on the verge of slipping, f1 f1 max s n1 s m m p g . Then Fx 0 n2 f1 , or n2 s m m p g . Finally, 0 n2 L sin m g (L/2) cos mp gx cos 0 where x is the maximum distance the painter can go up the ladder before it will start to slip. Solving for x gives L n2 L sin m g cos m m 2 x s 1 L tan L m p g cos mp 2m p and using the given numerical data, we find 30 kg 30 kg x 0.45 1 4.0 m tan 53 4.0 m 2.5 m 80 kg 2 80 kg 8.83 The large mass (m1 = 60.0 kg) moves in a circular path of radius r1 = 0.140 m, while the radius of the path for the small mass (m2 = 0.120 kg) is r2 r1 3.00 m 0.140 m 2.86 m The system has maximum angular speed when the rod is in the vertical position as shown at the right. We take PEg = 0 at the level of the horizontal Page 8.50 Chapter 8 rotation axis and use conservation of energy to find: KE f PEg f KEi PEg 1 1 2 2 2 I1 max 2 I 2 max m2 gr2 m1gr1 0 0 i Approximating the two objects as point masses, we have I1 m1r12 and I2 m2r22 . The energy conservation equation then becomes max 1 2 2 m1r1 m2r2 g m1r12 m2r22 max 2 m1r1 m2 r2 g m1r12 m2 r22 and yields 2 60.0 kg 0.140 m 0.120 kg 2.86 m 9.80 m s 2 60.0 kg 0.140 m 2 0.120 kg 2.86 m 2 or max 8.56 rad s . The maximum linear speed of the small mass object is then 2 max 8.84 (a) r2max 2.86 m 8.56 rad s 24.5 m s Note that the cylinder has both translational and rotational motion. The center of gravity accelerates downward while the cylinder rotates around the center of gravity. Thus, we apply both the translational and the rotational forms of Newton’s second law to the cylinder: Fy ma y T mg m a or T m g a I [1] Tr I a r For a uniform, solid cylinder, I 1 mr 2 so our last result becomes 2 mr 2 a 2T Tr or a 2 r m [2] Substituting Equation [2] into Equation [1] gives T = mg – 2T, and solving for T yields T = mg/3. (b) From Equation [2] above, Page 8.51 Chapter 8 2T 2 mg 2g 3 m m 3 a (c) Considering the translational motion of the center of gravity, 2y 02y 2ay y gives y 2g 0 2 h 3 4 gh 3 Using conservation of energy with PEg at the final level of the cylinder gives KE t KEr PEg Since y r and I yielding y 8.85 KEt KEr PEg f 1 2 mr 2 , this becomes i or 1 2 m2y 1 2 I 2 0 0 0 mgh 2 3 1 11 y m 2y m r 2 mgh , or m 2y mgh r 2 2 22 4 4 gh 3 . Considering the shoulder joint as the pivot, the second condition of equilibrium gives 0 w 70 cm Fm sin 45 4.0 cm 0 2 or Fm w 70 cm 2 4.0 cm sin 45 12.4 w Recall that this is the total force exerted on the arm by a set of two muscles. If we approximate that the two muscles of this pair exert equal magnitude forces, the force exerted by each muscle is Page 8.52 Chapter 8 Feach Fm 12.4 w 6.2 w 6.2 750 N 4.6 10 3 N 4.6 kN 2 2 muscle 8.86 Observe that since the torque opposing the rotational motion of the gymnast is constant, the work done by nonconservative forces as the gymnast goes from position 1 to position 2 (an angular displacement of /2 rad) will be the same as that done while the gymnast goes from position 2 to position 3 (another angular displacement of /2 rad). Choose PEg = 0 at the level of the bar, and let the distance from the bar to the center of gravity of the outstretched body be reg. Applying the work–energy theorem, Wnc KE PEg f KE PEg , to the rotation from posii tion 1 to position 2 gives Wnc 12 1 2 I 22 0 0 mgrcg or Wnc 12 1 2 I 22 mgrcg [1] Now, apply the work–energy theorem to the rotation from position 2 to position 3 to obtain Wnc 23 21 I 32 mg rcg 1 2 I 22 0 or Wnc 23 1 2 I 32 1 2 I 22 mgrcg [2] Since the frictional torque is constant and these two segments of the motion involve equal angular displacements, Wnc 23 Wnc 12 . Thus, equating Equation [2] to Equation [1] gives 1 2 I 32 1 2 I 22 mgrcg which yields 32 222 , or 3 8.87 (a) 1 2 I 22 mgrcg 22 2 4.0 rad s 5.7 rad s . Free-body diagrams for each block and the pulley are given at the right. Observe that the angular acceleration of the pulley will be clockwise in direction and has been given a negative sign. Since I , the positive sense for torques and angular acceleration must be the same (counterclockwise). For m1: Fy may T1 m1g m1 a Page 8.53 Chapter 8 T1 m1 g a [1] For m2: Fx max T2 m2 a [2] For the pulley: I T2r T1r I a r or I T1 T2 2 a r [3] Substitute Equations [1] and [2] into Equation [3] and solve for a to obtain a m1 g I m1 m2 r2 or a (b) 4.00 kg 9.80 m s2 0.500 kg m2 0.300 m 2 4.00 kg 3.00 kg 3.12 m s2 Equation [1] above gives: T1 4.00 kg 9.80 m s2 3.12 m s2 26.7 N , and Equation [2] yields: T2 3.00 kg 3.12 m s2 9.37 N . 8.88 (a) (b) Fy 0 nF 120 N mmonkey g 0 nF 120 N 10.0 kg 9.80 m s2 218 N (c) When x = 2L/3, we consider the bottom end of the ladder as our pivot and obtain bottom 0 end L 2L 120 N cos 60.0 98.0 N cos 60.0 nW L sin 60.0 0 2 3 or Page 8.54 Chapter 8 60.0 N 196 3 N cos 60.0 nW 72.4 N sin 60.0 Then, Fx 0 (d) T nW 0 or T nW 72.4 N 0 yields When the rope is ready to break, T nW 80.0 N . Then bottom end L 120 N cos 60.0 98.0 N x cos 60.0 80.0 N L sin 60.0 0 2 or 80.0 N sin 60.0 60.0 N cos 60.0 L x 0.802 L 0.802 3.00 m 2.41 m 98.0 N cos 60.0 (e) If the horizontal surface were rough and the rope removed, a horizontal static friction force directed toward the wall would act on the bottom end of the ladder. Otherwise, the analysis would be much as what is done above. The maximum distance the monkey could climb would correspond to the condition that the friction force have its maximum value, s nF , so you would need to know the coefficient of static friction to solve part (d). Page 8.55