CHAPTER 9 ROTATIONAL DYNAMICS PROBLEMS _________________________________________________________________________________________ ___ 1. SSM REASONING AND SOLUTION Solving Equation 9.1 for the lever arm l , we obtain τ 3.0 N ⋅ m = 0.25 m l= = F 12 N _________________________________________________________________________________________ ___ 2. REASONING The torque is given by Equation 9.1, τ = F l , where F is the magnitude of the applied force and l is the lever arm. From the figure in the text, the lever arm is given by l = ( 0.28 m) sin 50.0 ° . Since both τ and l are known, Equation 9.1 can be solved for F. SOLUTION Solving Equation 9.1 for F, we have F= τ 45 N ⋅ m = = 2.1 ×10 l (0.28 m) sin 50.0 ° 2 N _________________________________________________________________________________________ ___ 3. REASONING AND SOLUTION where L is the lever arm. The torque about the center of the cable car is τ = FL, τ = FL = 2(185 N)(4.60 m) = 1.70 × 10 3 N ⋅ m _________________________________________________________________________________________ ___ 4. REASONING To calculate the torques, we need to determine the lever arms for each of the forces. These lever arms are shown in the following drawings: Axis 2.50 m Axis 32.0° 32.0° 2.50 m lT = (2.50 m) cos 32.0° W lW = (2.50 m) sin 32.0° T SOLUTION a. Using Equation 9.1, we find that the magnitude of the torque due to the weight W is 320 ROTATIONAL DYNAMICS b gb g τ W = Wl W = 10 200 N 2 .5 m sin32 ° = 13 500 N ⋅ m b. Using Equation 9.1, we find that the magnitude of the torque due to the thrust T is b gb g τ T = Tl T = 62 300 N 2 .5 m cos 32 ° = 132 000 N ⋅ m _________________________________________________________________________________________ ___ 5. REASONING The torque on either wheel is given by Equation 9.1, τ = F l, where F is the magnitude of the force and l is the lever arm. Regardless of how the force is applied, the lever arm will be proportional to the radius of the wheel. SSM SOLUTION The ratio of the torque produced by the force in the truck to the torque produced in the car is τtruck τ car = F l truck F l car = Fr truck Fr car = rtruck r car = 0.25 m 0.19 m = 1.3 _________________________________________________________________________________________ ____ 6. REASONING To calculate the torque, we will need the lever arm of the 110 N force. The drawing identifies the lever arm l. 15° 3.0 m W =110 N SOLUTION According to Equation 9.1, the magnitude of the torque is b gb l = (3.0 m)cos 15° g τ = Wl = 110 N 3.0 m cos 15°= 320 N ⋅ m _________________________________________________________________________________________ ____ 7. REASONING AND SOLUTION The torque due to F1 is τ1 = −F1L1 = −(20.0 N)(0.500 m) = −10.0 N⋅m (CW) The torque due to F2 is τ2 = (F2 cos 30.0°)L2 = (35.0 N)(1.10 m) cos 30.0° = 33.3 N⋅m (CCW) The net torque is therefore, Chapter 9 Problems 321 Στ = τ1 + τ2 = −10.0 N⋅m + 33.3 N⋅m = 23.3 N ⋅ m, counterclockwise _________________________________________________________________________________________ ___ 8. REASONING AND SOLUTION The torque produced by a force of magnitude F is given by Equation 9.1, τ = F l, where l is the lever arm. In each case, the torque produced by the couple is equal to the sum of the individual torques produced by each member of the couple. a. When the axis passes through point A, the torque due to the force at A is zero. The lever arm for the force at C is L. Therefore, taking counterclockwise as the positive direction, we have τ = τ A + τC = 0 + τC = FL b. Each force produces a counterclockwise rotation. The magnitude of each force is F and each force has a lever arm of L / 2 . Taking counterclockwise as the positive direction, we have L L τ = τ A + τC = F + F = FL 2 2 c. When the axis passes through point C, the torque due to the force at C is zero. The lever arm for the force at A is L. Therefore, taking counterclockwise as the positive direction, we have τ = τ A + τC = τA + 0 = FL Note that the value of the torque produced by the couple is the same in all three cases; in other words, when the couple acts on the tire wrench, the couple produces a torque that does not depend on the location of the axis. _________________________________________________________________________________________ ___ 9. REASONING Since the meter stick does not move, it is in equilibrium. The forces and the torques, therefore, each add to zero. We can determine the location of the 6.00 N force, by using the condition that the sum of the torques must vectorially add to zero. SSM F pinned end 2 30.0° l2 l1 F TOP VIEW 1 SOLUTION If we take counterclockwise torques as positive, then the torque of the first force about the pin is τ 1 = F1 l 1 = (2.00 N)(1.00 m) = 2.00 N ⋅ m 322 ROTATIONAL DYNAMICS The torque due to the second force is τ 2 = – F2 (sin 30.0 ° ) l 2 = – (6.00 N)(sin 30.0 ° ) l 2 = –( 3.00 N) l 2 The torque τ 2 is negative because the force F2 tends to produce a clockwise rotation about the pinned end. Since the net torque is zero, we have 2 .00 N ⋅ m +[– ( 3.00 N) l 2 ] = 0 Thus, l2 = 2.00 N ⋅ m = 0.667 m 3.00 N _________________________________________________________________________________________ ___ 10. REASONING AND SOLUTION The net torque about the axis in text drawing (a) is Στ = τ1 + τ2 = F1b − F2a = 0. Considering that F2 = 3F1, we have b – 3a = 0. The net torque in drawing (b) is then Στ = F1(1.00 m − a) − F2b = 0 or 1.00 m − a − 3b = 0. Solving the first equation for b, substituting into the second equation and rearranging, gives a= 0.100 m 0.300 m and b = _________________________________________________________________________________________ ____ 11. REASONING AND SOLUTION a. Taking torques about an axis through the rear axle of the car gives 2Ff(2.54 m) − (1160 kg)(9.80 m/s2)(1.52 m) = 0 or Ff = 3.40 × 10 3 N Fr = 2.28 × 10 N b. Taking torques about an axis through the front axle gives (1160 kg)(9.80 m/s2)(1.02 m) − 2Fr(2.54 m) = 0 or 3 _________________________________________________________________________________________ ____ 12. REASONING The drawing shows the forces acting on the person. It also shows the lever arms for a rotational axis FHANDS FFEET Axis W Chapter 9 Problems 323 perpendicular to the plane of the paper at the place where the person’s toes touch the floor. Since the person is in equilibrium, the sum of the forces must be zero. Likewise, we know that the sum of the torques must be zero. SOLUTION Taking upward to be the positive direction, we have FFEET + FHANDS − W = 0 Remembering that counterclockwise torques are positive and using the axis and the lever arms shown in the drawing, we find Wl W − FHANDS l HANDS = 0 FHANDS = Wl W l HANDS = b584 N gb0 .840 mg= 392 N 1.250 m Substituting this value into the balance-of-forces equation, we find FFEET = W − FHANDS = 584 N − 392 N = 192 N The force on each hand is half the value calculated above, or 196 N . Likewise, the force on each foot is half the value calculated above, or 96 N . _________________________________________________________________________________________ ____ 13. REASONING The minimum value for the coefficient of static friction between the ladder and the ground, so that the ladder does not slip, is given by Equation 4.7: SSM f s MAX = µs FN SOLUTION From Example 4, the magnitude of the force of static friction is Gx = 727 N. The magnitude of the normal force applied to the ladder by the ground is Gy = 1230 N. The minimum value for the coefficient of static friction between the ladder and the ground is µs = f sMAX FN = Gx Gy = 727 N = 0 . 591 1230 N 324 ROTATIONAL DYNAMICS _________________________________________________________________________________________ ____ 14. REASONING When the board just begins to tip, three forces act on the board. They are the weight W of the board, the weight W P of the person, and the force F exerted by the right support. F 1.4 m x W = 225 N W P = 450 N Since the board will rotate around the right support, the lever arm for this force is zero, and the torque exerted by the right support is zero. The lever arm for the weight of the board is equal to one-half the length of the board minus the overhang length: 2.5 m – 1.1 m = 1.4 m . The lever arm for the weight of the person is x. Therefore, taking counterclockwise torques as positive, we have − W P x + W (1.4 m) = 0 This expression can be solved for x. SOLUTION Solving the expression above for x, we obtain x= W (1.4 m) WP = (225 N)(1.4 m) 450 N = 0.70 m _________________________________________________________________________________________ ____ Chapter 9 Problems 15. REASONING The figure at the right shows the door and the forces that act upon it. Since the door is uniform, the center of gravity, and, thus, the location of the weight W, is at the geometric center of the door. 325 SSM Let U represent the force applied to the door by the upper hinge, and L the force applied to the door by the lower hinge. Taking forces that point to the right and forces that point up as positive, we have ∑ Fx = L x − U x = 0 ∑ Fy = Ly − W = 0 or L x = U x or L y = W = 140 N U x h = 2.1 m W L y Lx (1) d = 0.81 m (2) Taking torques about an axis perpendicular to the plane of the door and through the lower hinge, with counterclockwise torques being positive, gives d ∑ τ = −W + U x h = 0 (3) 2 Equations (1), (2), and (3) can be used to find the force applied to the door by the hinges; Newton's third law can then be used to find the force applied by the door to the hinges. SOLUTION a. Solving Equation (3) for Ux gives Ux = Wd 2h = (140 N)(0.81 m) 2(2.1 m) = 27 N From Equation (1), Lx = 27 N. Therefore, the upper hinge exerts on the door a horizontal force of 27 N to the left . b. From Equation (1), Lx = 27 N, we conclude that the bottom hinge exerts on the door a horizontal force of 27 N to the right . c. From Newton's third law, the door applies a force of 27 N force points horizontally to the right on the upper hinge. This , according to Newton's third law. 326 ROTATIONAL DYNAMICS d. Let D represent the force applied by the door to the lower hinge. Then, from Newton's third law, the force exerted on the lower hinge by the door has components Dx = – 27 N and Dy = – 140 N. From the Pythagorean theorem, D D= D +D = 2 x 2 y ( −27 N) + ( −140 N) = 2 2 x 143 N θ The angle θ is given by θ = tan −1 D F–140 N I = 79 ° G H–27 N JK The force is directed 79 ° below the horizontal y . 16. REASONING AND SOLUTION The net torque about an axis through the contact point between the tray and the thumb is Στ = F(0.0400 m) − (0.250 kg)(9.80 m/s2)(0.320 m) − (1.00 kg)(9.80 m/s2)(0.180 m) − (0.200 kg)(9.80 m/s2)(0.140 m) = 0 F = 70.6 N, up Similarly, the net torque about an axis through the point of contact between the tray and the finger is Στ = T(0.0400 m) − (0.250 kg)(9.80 m/s2)(0.280 m) − (1.00 kg)(9.80 m/s2)(0.140 m) − (0.200 kg)(9.80 m/s2)(0.100 m) = 0 T = 56.4 N, down _________________________________________________________________________________________ ____ 17. REASONING AND SOLUTION When the arm is in equilibrium, the sum of the torques is zero. Taking torques about the elbow joint with counterclockwise torques taken as positive, we have − F lF + M lM = 0 Solving for M, lF 0.30 m M=F = 1.0 × 10 3 N = (170 N) 0.051 m lM The direction of the force is to the left . Chapter 9 Problems 327 _________________________________________________________________________________________ ____ 18. REASONING Although this arrangement of body parts is vertical, we can apply Equation 9.3 to locate the overall center of gravity by simply replacing the horizontal position x by the vertical position y, as measured relative to the floor. SOLUTION Using Equation 9.3, we have y cg = = W1 y1 + W2 y 2 + W3 y 3 W1 + W2 + W3 b438 N gb1. 28 mg+ b144 N gb0.760 m g+ b87 N gb0.250 m g= 438 N + 144 N + 87 N 1.03 m _________________________________________________________________________________________ ____ 19. REASONING The jet is in equilibrium, so the sum of the external forces is zero, and the sum of the external torques is zero. We can use these two conditions to evaluate the forces exerted on the wheels. SOLUTION a. Let Ff be the magnitude of the normal force that the ground exerts on the front wheel. Since the net torque acting on the plane is zero, we have (using an axis through the points of contact between the rear wheels and the ground) Στ = −W lw + Ff lf = 0 where W is the weight of the plane, and lw and lf are the lever arms for the forces W and Ff , respectively. Thus, Στ = −(1.00 × 106 N)(15.0 m − 12.6 m) + Ff (15.0 m) = 0 Solving for Ff gives Ff = 1.60 × 10 5 N . b. Setting the sum of the vertical forces equal to zero yields ΣFy = Ff + 2Fr − W = 0 where the factor of 2 arises because there are two rear wheels. Substituting in the data, ΣFy = 1.60 × 105 N + 2Fr − 1.00 × 106 N = 0 328 ROTATIONAL DYNAMICS Fr = 4.20 × 10 5 N _________________________________________________________________________________________ ____ 20. REASONING AND SOLUTION a. Taking torques about an axis through the bolt we have −(4.5 × 103 N)(2.50 m) − (12.0 × 103 N)(3.50 m) + T(5.00 m) sin 25.0° = 0 Solving for T yields T= 4 2.52 × 10 N b. Applying Newton's second law in the horizontal direction gives −T cos 25.0° + Fh = 0, so Fh = 2.28 × 104 N In the vertical direction Fv − WL − WB + T sin 25.0° = 0, and Fv = 5.85 × 103 N Now the force exerted on the beam by the bolt is F = Fh2 + F v2 = 2.35 × 10 4 N _________________________________________________________________________________________ ____ 21. REASONING AND SOLUTION The figure below shows the massless board and the forces that act on the board due to the person and the scales. SSM WWW 2.00 m person's feet person's head x center of gravity of person 425 N 315 N W a. Applying Newton's second law to the vertical direction gives 315 N + 425 N – W = 0 or W = 7.40 × 10 2 N, downward Chapter 9 Problems 329 b. Let x be the position of the center of gravity relative to the scale at the person's head. Taking torques about an axis through the contact point between the scale at the person's head and the board gives (315 N)(2.00 m) – (7.40 × 102 N)x = 0 x = 0.851 m or _________________________________________________________________________________________ ____ 22. REASONING AND SOLUTION The net torque about an axis through the knee joint is Στ = M(sin 25.0°)(0.100 m) − (44.5 N)(cos 30.0°)(0.250 m) = 0 M = 228 N _________________________________________________________________________________________ ____ 23. REASONING Since the man holds the ball motionless, the ball and the arm are in equilibrium. Therefore, the net force, as well as the net torque about any axis, must be zero. SSM SOLUTION a. Using Equation 9.1, the net torque about an axis through the elbow joint is Στ = M(0.0510 m) – (22.0 N)(0.140 m) – (178 N)(0.330 m) = 0 Solving this expression for M gives M = 1.21 × 10 3 N . b. The net torque about an axis through the center of gravity is Στ = – (1210 N)(0.0890 m) + F(0.140 m) – (178 N)(0.190 m) = 0 Solving this expression for F gives F = 1.01 × 10 3 N . Since the forces must add to give a net force of zero, we know that the direction of F is downward . _________________________________________________________________________________________ ____ 24. REASONING If we assume that the system is in equilibrium, we know that the vector sum of all the forces, as well as the vector sum of all the torques, that act on the system must be zero. The figure below shows a free body diagram for the boom. Since the boom is assumed to be uniform, its weight W B is located at its center of gravity, which coincides with its geometrical center. There is a tension T in the cable that acts at an angle θ to the horizontal, as shown. At the hinge pin P, there are two forces acting. The vertical force V that acts on the end of the boom 330 ROTATIONAL DYNAMICS prevents the boom from falling down. The horizontal force H that also acts at the hinge pin prevents the boom from sliding to the left. The weight W L of the wrecking ball (the "load") acts at the end of the boom. θ= 32° T φ– θ WB V θ= 32° WL P φ= 48° H By applying the equilibrium conditions to the boom, we can determine the desired forces. SOLUTION The directions upward and to the right will be taken as the positive directions. In the x direction we have ∑ Fx = H − T cos θ = 0 (1) while in the y direction we have ∑ Fy = V − T sin θ − WL − WB = 0 (2) Equations (1) and (2) give us two equations in three unknown. We must, therefore, find a third equation that can be used to determine one of the unknowns. We can get the third equation from the torque equation. In order to write the torque equation, we must first pick an axis of rotation and determine the lever arms for the forces involved. Since both V and H are unknown, we can eliminate them from the torque equation by picking the rotation axis through the point P (then both V and H have zero lever arms). If we let the boom have a length L, then the lever arm for W L is L cos φ , while the lever arm for W B is ( L / 2) cos φ . From the figure, we see that the lever arm for T is L sin( φ – θ) . If we take counterclockwise torques as positive, then the torque equation is L cos φ ∑ τ = −WB − W L L cos φ+ TL sin (φ −θ ) = 0 2 Solving for T, we have T = 1 2 WB + WL sin( φ – θ ) cos φ (3) Chapter 9 Problems 331 a. From Equation (3) the tension in the support cable is T = 1 2 (3600 N) + 4800 N sin(48 ° – 32 °) cos 48 ° = 1.6 × 10 4 N b. The force exerted on the lower end of the hinge at the point P is the vector sum of the forces H and V. According to Equation (1), ( H = T cos θ = 1.6 ×10 4 ) N cos 32 ° = 1.4 × 10 4 N and, from Equation (2) ( ) V = W L + W B + T sin θ = 4800 N + 3600 N + 1.6 × 10 4 N sin 32 ° = 1.7 × 10 4 N Since the forces H and V are at right angles to each other, the magnitude of their vector sum can be found from the Pythagorean theorem: FP = H 2 + V 2 = (1.4 × 10 4 N) 2 + (1.7 × 10 4 N) 2 = 2.2 × 10 4 N _________________________________________________________________________________________ ____ 25. REASONING AND SOLUTION Taking torques on the right leg about the apex of the “A” gives Στ = −(120 N) L cos 60.0° − FL cos 30.0° + T(2L) cos 60.0° = 0 where F is the horizontal component of the force exerted by the crossbar and T is the tension in the right string. Due to symmetry, the tension in the left string is also T. Newton's second law applied to the vertical gives 2T − 2W = 0 so T = 120 N Substituting T = 120 N into the first equation yields F = 69 N . _________________________________________________________________________________________ ____ ROTATIONAL DYNAMICS 332 26. REASONING The drawing shows the forces acting on the board, which has a length L. Wall 2 exerts a normal force P2 on the lower end of the board. The maximum force of static friction that wall 2 can apply to the lower end of the board is µs P2 and is directed upward in the drawing. The weight W acts downward at the board's center. Wall 1 applies a normal force P1 to the upper end of the board. We take upward and to the right as our positive directions. P Wall 1 1 Wall 2 µ s P2 W θ P2 SOLUTION Then, since the horizontal forces balance to zero, we have P 1 – P2 = 0 (1) µs P2 – W = 0 (2) The vertical forces also balance to zero: Using an axis through the lower end of the board, we now balance the torques to zero: L (cos θ ) − P1 L (sin θ ) = 0 2 W Rearranging Equation (3) gives W tan θ = (3) (4) 2P1 But W = µs P2 according to Equation (2), and P2 = P1 according to Equation (1). Therefore, W = µs P1, which can be substituted in Equation (4) to show that tan θ = µ s P1 2P1 = µs 2 = 0.98 2 or θ = tan–1(0.49) = 26° Chapter 9 Problems 333 From the drawing at the right, cos θ = d L L Therefore, the longest board that can be propped between the two walls is L= d 1.5 m = = cos θ cos 26 ° θ d 1.7 m _________________________________________________________________________________________ ____ 27. REASONING AND SOLUTION The weight W of the left side of the ladder, the normal force FN of the floor on the left leg of the ladder, the tension T in the crossbar, and the reaction force R due to the right-hand side of the ladder, are shown in the figure below. In the vertical direction −W + FN = 0, so that FN = W = mg = (10.0 kg)(9.80 m/s2) = 98.0 N R In the horizontal direction it is clear that R = T. The net torque about the base of the ladder is 75.0 Στ = – T [(1.00 m) sin 75.0o] – W [(2.00 m) cos 75.0o] + R [(4.00 m) sin 75.0o] = 0 W F Substituting for W and using R = T, we obtain T = (98.0 N )(2.00 m) cos 75.0 ° (3.00 m) s in 75.0 ° o N T = 17.5 N _________________________________________________________________________________________ ____ 28. REASONING The moment of inertia of the stool is the sum of the individual moments of inertia of its parts. According to Table 9.1, a circular disk of radius R has a moment of inertia of Idisk = 21 Mdisk R2 with respect to an axis perpendicular to the disk center. Each thin rod is attached perpendicular to the disk at its outer edge. Therefore, each particle in a rod is located at a perpendicular distance from the axis that is equal to the radius of the disk. This means that each of the rods has a moment of inertia of Irod = Mrod R2. SOLUTION Remembering that the stool has three legs, we find that the its moment of inertia is 334 ROTATIONAL DYNAMICS I stool = I disk + 3 I rod = 12 M disk R 2 + 3 M rod R 2 = 1 2 b1.2 kg gb0.16 mg + 3b0.15 kg gb0 .16 m g = 2 2 0. 027 kg ⋅ m 2 ______________________________________________________________________________ 29. REASONING AND SOLUTION For a rigid body rotating about a fixed axis, Newton's second law for rotational motion is given by Equation 9.7, ∑ τ = I α, where I is the moment of inertia of the body and α is the angular acceleration expressed in rad/s2. Equation 9.7 gives SSM I= ∑τ α = 10 .0 N ⋅ m 8.00 rad/s 2 = 1.25 kg ⋅ m 2 _________________________________________________________________________________________ ____ 30. REASONING AND SOLUTION We know Στ = Iα = (0.16 kg⋅m2)(7.0 rad/s2) = 1.1 kg⋅m2/s2 = 1.1 N ⋅ m _________________________________________________________________________________________ ____ 31. REASONING AND SOLUTION a. The net torque on the disk about the axle is Στ = F1R − F2R = (0.314 m)(90.0 N − 125 N) = − 11 N ⋅ m b. The angular acceleration is given by α = Στ/I. From Table 9.1, the moment of inertia of the disk is I = (1/2) MR2 = (1/2)(24.3 kg)(0.314 m) 2 = 1.20 kg⋅m2 α = (−11 N⋅m)/(1.20 kg⋅m2) = –9.2 rad / s 2 _________________________________________________________________________________________ ____ 32. REASONING The rotational analog of Newton's second law is given by Equation 9.7, ∑ τ = I α. Since the person pushes on the outer edge of one pane of the door with a force F that is directed perpendicular to the pane, the torque exerted on the door has a magnitude of FL, where the lever arm L is equal to the width of one pane of the door. Once the moment of inertia is known, Equation 9.7 can be solved for the angular acceleration α. Chapter 9 Problems 335 The moment of inertia of the door relative to the rotation axis is I = 4 IP , where IP is the moment 1 of inertia for one pane. According to Table 9.1, we find IP = 3 ML 2 , so that the rotational inertia 4 of the door is I = 3 ML 2 . SOLUTION Solving Equation 9.7 for α, and using the expression for I determined above, we have α= FL 4 3 ML = 2 F 4 3 ML = 68 N 4 3 (85 kg)(1.2 m) = 0.50 rad/s 2 _________________________________________________________________________________________ ____ 33. REASONING The figure below shows eight particles, each one located at a different corner of an imaginary cube. As shown, if we consider an axis that lies along one edge of the cube, two of the particles lie on the axis, and for these particles r = 0. The next four particles closest to the axis have r = l , where l is the length of one edge of the cube. The remaining two particles have r = d , where d is the length of the diagonal along any one of the faces. From the Pythagorean theorem, d = l 2 + l 2 = l 2 . SSM l Axis d d l l l According to Equation 9.6, the moment of inertia of a system of particles is given by I = ∑ mr 2 . SOLUTION Direct application of Equation 9.6 gives I = ∑ mr 2 = 4(m l2 ) + 2(md 2 ) = 4(m l 2 ) + 2(2m l 2 ) = 8m l2 or I = 8( 0.12 kg)(0.25 m) 2 = 0.060 kg ⋅ m 2 _________________________________________________________________________________________ ____ 34. REASONING AND SOLUTION 336 ROTATIONAL DYNAMICS a. We know that α = (ω – ωo)/t. But ω = (1/2)ωo, so α = −(1/2)ωo/t = −(1/2)(88.0 rad/s)/(5.00 s) = −8.80 rad/s2 The magnitude of α is 8.80 rad/s 2 . b. Στ = Iα and FR = Iα. The magnitude of the frictional force is F = Iα/R = (0.850 kg⋅m2)(8.80 rad/s2)/(0.0750 m) = 99.7 N _________________________________________________________________________________________ ____ 35. REASONING AND SOLUTION We know Στ = Iα, where I = (1/2) mr 2 = (1/2)(0.400 kg)(0.130 m) 2 = 3.38 × 10–3 kg⋅m2 Also, ω = ωo + αt, so that α = (85.0 rad/s − 262 rad/s)/(18.0 s) = −9.83 rad/s2. Thus, the net torque is Στ = Iα = (3.38 × 10–3 kg⋅m2)(−9.83 rad/s2) = − 3.32 × 10 –2 N ⋅ m _________________________________________________________________________________________ ____ 36. REASONING The force applied to the baton creates a net torque that gives the rod an angular acceleration, according to Newton’s second law as expressed for rotational motion (Στ = Iα). From the data given, we will calculate the moment of inertia I and the angular acceleration α. Newton’s second law, then, will allow us to obtain the net torque Στ. From the net torque, we will be able to determine the force, since the magnitude of the torque in this case is just the magnitude of the force times the lever arm of 2.0 cm. SOLUTION The momentum of inertia of the baton is the sum of the individual moments of inertia of its parts. For a thin rod of length L rotating about an axis perpendicular to the rod at its center, the moment of inertia is I rod = 121 M rod L2 . For each ball (assumed to be very small compared to the length of the rod), the moment of inertia is Iball = Mball (L/2)2. The total moment of inertia, then, is I baton = I rod + 2 I ball = 121 M rod L2 + 2 M ball c Lh = 1 2 2 1 12 M rod L2 + 21 M ball L2 Using Equation 8.4 from the equations of kinematics for rotational motion, we can determine the angular acceleration as Chapter 9 Problems α= 337 ω − ω0 t where ω and ω0 are, respectively, the final and initial angular velocities. Since only one force of magnitude F creates the torque and since Equation 9.1 gives the magnitude of the torque as the magnitude of the force times the lever arm l, Newton’s second law becomes Στ = Fl= Iα. Substituting our expressions for the moment of inertia and angular acceleration of the baton into the second law gives Fl = I baton α = c 1 12 M rod L2 + 12 M ball L2 ω− ω I hF G H t JK 0 In Newton’s second law the angular acceleration α must be expressed in rad/s2. Therefore, the values for the angular speeds ω and ω0 must be expressed in rad/s. Recognizing that 2.0 rev/s is 4.0 π rad/s and solving for F, we find that F= = c hFω − ω I G l H t JK b0 .13 kg gb0.81 mg + b0.13 kg gb0 .81 mg F 4 π rad / s − 0 rad / s I G JK= H 0.40 s 0.020 m 1 12 1 12 M rod L2 + 12 M ball L2 2 0 2 1 2 78 N _________________________________________________________________________________________ ____ 37. REASONING AND SOLUTION a. From Table 9.1 in the text, the moment of inertia of the rod relative to an axis that is perpendicular to the rod at one end is given by SSM I rod = 13 ML2 = 13 ( 2 .00 kg)(2.00 m) 2 = 2 .67 kg ⋅ m 2 b. The moment of inertia of a point particle of mass m relative to a rotation axis located a perpendicular distance r from the particle is I = mr 2 . Suppose that all the mass of the rod were located at a single point located a perpendicular distance R from the axis in part (a). If this point particle has the same moment of inertia as the rod in part (a), then the distance R, the radius of gyration, is given by R= I = m 2.67 kg ⋅ m 2 = 1.16 m 2.00 kg _________________________________________________________________________________________ ____ 338 ROTATIONAL DYNAMICS 38. REASONING AND SOLUTION The final angular speed of the arm is ω = vT/r, where r = 0.28 m. The angular acceleration needed to produce this angular speed is α = (ω − ω0)/t. The net torque required is Στ = Iα. This torque is due solely to the force M, so that Στ = ML. Thus, ω − ω0 I t ∑τ M= = L L F G H I JK Setting ω0 = 0 and ω = vT/r, the force becomes I M= Fv I G Hr t JK= Iv T L c0. 065 kg ⋅ m hb5.0 m / sg= = Lr t b 0. 025 m g b0.28 mgb0.10 sg 2 T 460 N _________________________________________________________________________________________ ____ 39. REASONING The angular acceleration of the bicycle wheel can be calculated from Equation 8.4. Once the angular acceleration is known, Equation 9.7 can be used to find the net torque caused by the brake pads. The normal force can be calculated from the torque using Equation 9.1. SSM SOLUTION The angular acceleration of the wheel is, according to Equation 8.4, α= ω − ω0 t = 3.7 rad/s − 13 .1 rad/s 3.0 s 2 = −3.1 rad/s If we assume that all the mass of the wheel is concentrated in the rim, we may treat the wheel as a hollow cylinder. From Table 9.1, we know that the moment of inertia of a hollow cylinder of mass m and radius r about an axis through its center is I = mr 2 . The net torque that acts on the wheel due to the brake pads is, therefore, 2 ∑ τ = I α= (mr ) α (1) From Equation 9.1, the net torque that acts on the wheel due to the action of the two brake pads is ∑ τ = –2 fk l (2) where f k is the kinetic frictional force applied to the wheel by each brake pad, and l = 0.33 m is the lever arm between the axle of the wheel and the brake pad (see the drawing in the text). The factor of 2 accounts for the fact that there are two brake pads. The minus sign arises because the net torque must have the same sign as the angular acceleration. The kinetic frictional force can be written as (see Equation 4.8) f k = µk FN (3) Chapter 9 Problems 339 where µk is the coefficient of kinetic friction and FN is the magnitude of the normal force applied to the wheel by each brake pad. Combining Equations (1), (2), and (3) gives 2 –2(µk FN ) l = (mr )α FN = – mr 2 α 2 µk l = –(1.3 kg)(0.33 m) 2 (–3.1 rad/s 2(0.85) ( 0.33 m) 2 ) = 0.78 N _________________________________________________________________________________________ ____ 40. REASONING AND SOLUTION The moment of inertia of a solid cylinder about an axis coinciding with the cylinder axis which contains the center of mass is Icm = (1/2) MR2. The parallel axis theorem applied to an axis on the surface (h = R) gives I = Icm + MR2, so that I= 3 2 MR 2 _________________________________________________________________________________________ ____ 41. REASONING AND SOLUTION For door A, θ = (1/2) α A tA 2. For door B, θ = (1/2) α BtB2. Equating gives αA t B = tA αB We need the angular accelerations. Applying Newton's second law for rotation to door A FL = (1/3)ML2α A and to door B F(1/2)L = (1/12)ML2α B Division of the previous two equations yields α A /α B = 1/2. Now tB = tA / 2 = (3.00 s)/(1.41) = 2.12 s _________________________________________________________________________________________ ____ 42. REASONING The drawing shows the drum, pulley, and the crate, as well as the tensions in the cord 340 ROTATIONAL DYNAMICS r2 T1 Pulley m 2 T2 = 1 3 0 kg T2 T1 r1 Cr a t e Dr u m m 3 = 1 8 0 kg m1 = 150 kg r 1 = 0 .7 6 m Let T1 represent the magnitude of the tension in the cord between the drum and the pulley. Then, the net torque exerted on the drum must be, according to Equation 9.7, Στ = I1α 1, where I1 is the moment of inertia of the drum, and α 1 is its angular acceleration. If we assume that the cable does not slip, then Equation 9.7 can be written as FI hG H JK a − T1 r1 + τ = m1 r12 14243 123 r1 23 ∑τ I 1 1α 1 c (1) where τ is the counterclockwise torque provided by the motor, and a is the acceleration of the cord (a = 1.2 m/s2). This equation cannot be solved for τ directly, because the tension T1 is not known. We next apply Newton’s second law for rotational motion to the pulley in the drawing: FI hG H JK a + T1 r2 − T2 r2 = 12 m2 r22 144244 3 1 424 3 r2 123 I2 ∑τ α2 c (2) where T2 is the magnitude of the tension in the cord between the pulley and the crate, and I2 is the moment of inertial of the pulley. Finally, Newton’s second law for translational motion (ΣFy = m a) is applied to the crate, yielding + T2 − m3 g = m3 a 14 4244 3 ∑ Fy (3) Chapter 9 Problems 341 SOLUTION Solving Equation (1) for T1 and substituting the result into Equation (2), then solving Equation (2) for T2 and substituting the result into Equation (3), results in the following value for the torque c h ) c150 kg + τ = r1 a m1 + 21 m2 + m3 + m3 g = ( 0. 76 m) (1.2 m / s 2 h 130 kg + 180 kg + ( 180 kg)(9.80 m / s 2 ) = 1700 N ⋅ m 1 2 _________________________________________________________________________________________ ____ 43. REASONING The kinetic energy of the flywheel is given by Equation 9.9. The moment of inertia of the flywheel is the same as that of a solid disk, and, according to Table 9.1 in the text, is given by I = 12 MR 2 . Once the moment of inertia of the flywheel is known, Equation 9.9 can be solved for the angular speed ω in rad/s. This quantity can then be converted to rev/min. SSM SOLUTION Solving Equation 9.9 for ω, we obtain, 2 ( KE R ) ω= I = 2 ( KE R ) 1 2 MR 2 = 4(1.2 × 10 9 J) = 6.4 × 10 4 rad / s 2 (13 kg)(0.30 m) Converting this answer into rev/min, we find that c ω = 6.4 × 10 4 rad / s 1 rev I F60 s I hF G H2 π rad JKG H1 min JK= 6.1 × 10 5 rev / min _________________________________________________________________________________________ ____ 44. REASONING The rotational kinetic energy of each object is given by Equation 9.9, KE R = 12 Iω2 . To solve this problem, we need only set the two kinetic energies equal, being sure to use the proper moment of inertia for each object, as given in Table 9.1. SOLUTION According to Table 9.1 the moment of inertia of the solid sphere is I solid = MR , while the moment of inertia of the shell is I shell = 23 MR 2 . Using these expressions in Equation 9.9 for the rotational kinetic energy, we obtain 2 5 2 ROTATIONAL DYNAMICS 342 I solid ω2solid = 12 I shell ω2shell 14243 14243 1 2 Rotational KE of solid sphere 1 2 c MR hω 2 5 2 2 5 ωsolid = 5 3 Rotational KE of spherical shell 2 solid = 1 2 c MR hω 2 3 2 2 shell ω2solid = 23 ω2shell ωshell = 5 3 b7. 0 rad / sg= 9. 0 rad / s _________________________________________________________________________________________ ____ 45. SSM REASONING AND SOLUTION a. The tangential speed of each object is given by Equation 8.9, v T = rω. Therefore, For object 1: v T1 = (2.00 m)(6.00 rad/s) = 12.0 m / s For object 2: v T2 = (1.50 m)(6.00 rad/s) = 9.00 m / s For object 3: v T3 = (3.00 m)(6.00 rad/s) = 18.0 m / s b. The total kinetic energy of this system can be calculated by computing the sum of the kinetic energies of each object in the system. Therefore, KE = 12 m1 v 12 + 12 m2 v 22 + 12 m3 v 32 KE = 1 2 ( 6. 00 kg)(12.0 m / s) 2 + ( 4 . 00 kg)(9.00 m / s) 2 + ( 3.00 kg)(18.0 m / s) 2 = 1.08 × 10 3 J c. The total moment of inertia of this system can be calculated by computing the sum of the moments of inertia of each object in the system. Therefore, I = ∑ mr 2 = m1 r12 + m2 r22 + m3 r32 I = ( 6 .00 kg)(2.00 m) 2 + ( 4 .00 kg)(1.50 m) 2 + ( 3. 00 kg)(3.00 m) 2 = 60. 0 kg ⋅ m 2 d. The rotational kinetic energy of the system is, according to Equation 9.9, KE R = 21 Iω2 = 12 (60.0 kg ⋅ m 2 )(6.00 rad / s) 2 = 1.08 × 10 3 J This agrees, as it should, with the result for part (b). Chapter 9 Problems 343 _________________________________________________________________________________________ ____ 46. REASONING a. The kinetic energy is given by Equation 9.9 as KE R = 12 Iω2 . Assuming the earth to be a uniform solid sphere, we find from Table 9.1 that the moment of inertia is I = 2 5 MR 2 . The mass and radius of the earth is M = 5.98 × 1024 kg and R = 6.38 × 106 m (see the inside of the text’s front cover). The angular speed ω must be expressed in rad/s, and we note that the earth turns once around its axis each day, which corresponds to 2π rad/day. b. The kinetic energy for the earth’s motion around the sun can be obtained from Equation 9.9 as KE R = 12 Iω2 . Since the earth’s radius is small compared to the radius of the earth’s orbit (Rorbit = 1.50 × 1011 m, see the inside of the text’s front cover), the moment of inertia in this case 2 is just I = MR orbit . The angular speed ω of the earth as it goes around the sun can be obtained from the fact that it makes one revolution each year, which corresponds to 2π rad/year. SOLUTION a. According to Equation 9.9, we have KE R = 21 Iω2 = 1 2 c MR hω 2 2 5 2 LF2 π rad I F1 day IF 1 h IO mh M G JP G J G J NH1 day KH24 h KH3600 s KQ 2 = 1 2 2 5 c5.98 × 10 24 hc kg 6. 38 × 10 6 2 = 2 .57 × 10 29 J b. According to Equation 9.9, we have KE R = 21 Iω2 = 1 2 cMR hω 2 orbit 2 LF2 π rad I F 1 yr I F1 day I F 1 h I O mh M H24 h JKG H3600 s JKP H1 yr JKG H365 day JKG NG Q 2 = 1 2 c5. 98 × 10 24 hc kg 1.50 × 10 11 2 = 2 .67 × 10 33 J _________________________________________________________________________________________ ____ 47. REASONING AND SOLUTION The conservation of energy gives for the cube (1/2) mvc2 = mgh, so vc = 2gh . The conservation of energy gives for the marble (1/2) mvm2 + (1/2) Iω2 = mgh. Since the marble rolls without slipping: ω = v/R. For a solid sphere we know I = (2/5) mR 2. Combining the last three equations gives 344 ROTATIONAL DYNAMICS vm = 10gh 7 = 7 = 1.18 5 Thus, vc vm _________________________________________________________________________________________ ____ The rotational kinetic energy of the shell is KEr = (1/2) Iω2 and the translational kinetic energy is KEt = (1/2) Mv2. Now, v = Rω since the sphere rolls without slipping, so KEt = (1/2) MR2ω2 The desired fraction is KEr/KE = I/(I + MR2) = 2/5 48. REASONING AND SOLUTION _________________________________________________________________________________________ ____ 49. REASONING AND SOLUTION The only force that does work on the cylinders as they move up the incline is the conservative force of gravity; hence, the total mechanical energy is conserved as the cylinders ascend the incline. We will let h = 0 on the horizontal plane at the bottom of the incline. Applying the principle of conservation of mechanical energy to the solid cylinder, we have 1 1 2 2 mgh s = 2 mv 0 + 2 Is ω0 (1) SSM 1 2 where, from Table 9.1, Is = 2 mr . In this expression, v 0 and ω0 are the initial translational and rotational speeds, and hs is the final height attained by the solid cylinder. Since the cylinder rolls without slipping, the rotational speed ω0 and the translational speed v 0 are related according to Equation 8.12, ω0 = v 0 / r . Then, solving Equation (1) for hs , we obtain hs = 3 v 02 4g Repeating the above for the hollow cylinder and using Ih = mr 2 we have hh = v 20 g The height h attained by each cylinder is related to the distance s traveled along the incline and the angle θ of the incline by Chapter 9 Problems ss = hs sin θ Dividing these gives sh = and ss 345 hh sin θ = 3/4 sh _________________________________________________________________________________________ ____ 50. REASONING AND SOLUTION The conservation of energy gives mgh + (1/2) mv2 + (1/2) Iω2 = (1/2) mvo2 + (1/2) Iωo2 If the ball rolls without slipping, ω = v/R and ωo = vo/R. We also know I = (2/5) mR 2. Substitution of the last two equations into the first and rearrangement gives v= v 20 − 10 7 gh = b3.50 m / sg − c9 .80 m / s hb0 .760 m g= 2 2 10 7 1.3 m / s _________________________________________________________________________________________ ____ 51. REASONING We first find the speed v 0 of the ball when it becomes airborne using the conservation of mechanical energy. Once v 0 is known, we can use the equations of kinematics to find its range x. SOLUTION When the tennis ball starts from rest, its total mechanical energy is in the form of gravitational potential energy. The gravitational potential energy is equal to mgh if we take h = 0 at the height where the ball becomes airborne. Just before the ball becomes airborne, its mechanical energy is in the form of rotational kinetic energy and translational kinetic energy. At 1 1 this instant its total energy is 2 mv 20 + 2 Iω2 . If we treat the tennis ball as a thin-walled spherical shell of mass m and radius r, and take into account that the ball rolls down the hill without slipping, its total kinetic energy can be written as 1 2 2 mv 0 + 1 2 2 Iω = 1 2 2 mv 0 + 1 2 2 2 ( mr ) 3 2 5 v0 2 = mv 0 r 6 Therefore, from conservation of mechanical energy, he have mgh = 5 6 2 mv 0 or v0 = 6 gh 5 The range of the tennis ball is given by x = v0 x t = v 0 (cos θ ) t , where t is the flight time of the ball. From Equation 3.3b, we find that the flight time t is given by 346 ROTATIONAL DYNAMICS t = v − v0 y ay = ( −v 0 y ) − v 0 y ay =– 2v 0 sin θ ay Therefore, the range of the tennis ball is 2v0 sin θ ay x = v0 x t = v0 (cos θ) – If we take upward as the positive direction, then using the fact that a y = – g and the expression for v 0 given above, we find 2 cos θ sin θ 2 2 cos θ sin θ 6 gh 2 12 x = v0 = = h cos θ sin θ g g 5 5 = 12 (1.8 m) (cos 35 °)(sin 35 ° ) = 2.0 m 5 _________________________________________________________________________________________ ____ 52. REASONING AND SOLUTION The angular momentum of the satellite is conserved if only the gravitational force of the earth is acting on it. We have LA = LP or mv A rA = mv PrP. Now rP = (v A /v P)rA = (1/1.20)(1.30 × 107 m) = 1.08 × 10 7 m _________________________________________________________________________________________ ____ 53. SSM WWW REASONING Let the two disks constitute the system. Since there are no external torques acting on the system, the principle of conservation of angular momentum applies. Therefore we have Linitial = Lfinal , or I A ω A + I Bω B = ( I A + I B ) ωfinal This expression can be solved for the moment of inertia of disk B. SOLUTION Solving the above expression for I B , we obtain I B = IA Fω G Hω final B – ωA – ωfinal I = ( 3.4 kg ⋅ m ) L –2.4 rad / s – 7.2 rad / s O= JK M N–9.8 rad / s – (–2.4 rad / s) P Q 2 4.4 kg ⋅ m 2 _________________________________________________________________________________________ ____ 54. REASONING AND SOLUTION Angular momentum is conserved, Iω = I0ω0, so Chapter 9 Problems FI I F5.40 kg ⋅ m Ib5.00 rad / sg= ω = G Jω = G HI K H3.80 kg ⋅ m JK 347 2 0 0 2 7 .11 rad / s _________________________________________________________________________________________ ____ 55. REASONING AND SOLUTION a. Angular momentum is conserved, so that Iω = Ioωo, where I = Io + 10mbRb2 = 2100 kg⋅m2 ω = (Io/I)ωo = [(1500 kg⋅m2)/(2100 kg⋅m2)](0.20 rad/s) = 0.14 rad/s b. A net external torque must be applied in a direction that is opposite to the angular deceleration caused by the baggage dropping onto the carousel. _________________________________________________________________________________________ ____ 56. REASONING AND SOLUTION The conservation of angular momentum applies about the indicated axis Idωd + MpRp2ωp = 0 where ωp = vp/Rp Now Id = (1/2) MdRd2. Combining and solving yields ωd = −2(Mp/Md)(Rp/Rd2)vp = −2 F 40.0 kg I L 1.25 m O M Pb2 .00 m / sg= −0.500 rad/s G J H1.00 × 10 kg KM Nb2.00 m g P Q The magnitude of ωd is 0.500 rad/s 2 2 . The negative sign indicates that the disk rotates in a direction opposite to the motion of the person. _________________________________________________________________________________________ ____ 57. REASONING Let the space station and the people within it constitute the system. Then as the people move radially from the outer surface of the cylinder toward the axis, any torques that occur are internal torques. Since there are no external torques acting on the system, the principle of conservation of angular momentum can be employed. SSM SOLUTION Since angular momentum is conserved, I final ω final = I 0ω0 ROTATIONAL DYNAMICS 348 Before the people move from the outer rim, the moment of inertia is 2 I 0 = I station + 500 mperson rperson or I 0 = 3.00 × 10 9 kg ⋅ m 2 + ( 500)(70.0 kg)(82.5 m) 2 = 3.24 × 10 9 kg ⋅ m 2 If the people all move to the center of the space station, the total moment of inertia is I final = I station = 3.00 × 10 9 kg ⋅ m 2 Therefore, ωfinal ω0 = I0 I final = 3.24 × 10 9 kg ⋅ m 2 = 1. 08 3.00 × 10 9 kg ⋅ m 2 This fraction represents a percentage increase of 8 percent . _________________________________________________________________________________________ ____ 58. REASONING When the modules pull together, they do so by means of forces that are internal. These pulling forces, therefore, do not create a net external torque, and the angular momentum of the system is conserved. In other words, it remains constant. We will use the conservation of angular momentum to obtain a relationship between the initial and final angular speeds. Then, we will use Equation 8.9 (v = rω) to relate the angular speeds ω0 and ωf to the tangential speeds v 0 and v f. SOLUTION Let L be the initial length of the cable between the modules and ω0 be the initial angular speed. Relative to the center-of-mass axis, the initial momentum of inertia of the twomodule system is I0 = 2M(L/2)2, according to Equation 9.6. After the modules pull together, the length of the cable is L/2, the final angular speed is ωf, and the momentum of inertia is If = 2M(L/4)2. The conservation of angular momentum indicates that I f ω f = I 0ω0 12 3 123 Final angular momentum L2 M FL I O JKPω M G H 4 M P N Q 2 f Initial angular momentum L FL I O JKPω M G H 2 M P N Q 2 = 2M 0 ωf = 4 ω0 According to Equation 8.9, ωf = v f/(L/4) and ω0 = v 0/(L/2). With these substitutions, the result that ωf = 4ω0 becomes Chapter 9 Problems vf L/4 =4 Fv I G HL / 2 JK 0 or b 349 g v f = 2 v 0 = 2 17 m / s = 34 m / s _________________________________________________________________________________________ ____ 59. REASONING AND SOLUTION After the mass has moved inward to its final path the centripetal force acting on it is T = 105 N. r 10 5 N Its centripetal acceleration is ac = v 2/R = T/m Now v = ωR so R = T/(ω2m) The centripetal force is parallel to the line of action (the string), so the force produces no torque on the object. Hence, angular momentum is conserved. Iω = Ioωo so that ω = (Io/I)ωo = (Ro2/R2)ωo Substituting and simplifying R3 = (mRo4 ωo2)/T, so that R = 0.573 m _________________________________________________________________________________________ ____ 60. REASONING AND SOLUTION The block will just start to move when the centripetal force on the block just exceeds f smax . Thus, if rf is the smallest distance from the axis at which the block stays at rest when the angular speed of the block is ωf, then µs FN = mrf ωf2, or µs mg = mrf ωf2 µs g = rf ωf2 (1) 350 ROTATIONAL DYNAMICS Since there are no external torques acting on the system, angular momentum will be conserved. I0 ω0 = If ωf where I0 = mr02, and If = mrf2. Making these substitutions yields r02 ω0 = rf2 ωf (2) Solving Equation (2) for ωf and substituting into Equation (1) yields: 2 µ s g = rf ω 0 r04 r f4 Solving for rf gives ω 2 r 4 1/3 (2.2 rad/s) 2 (0.30 m) 4 1/3 0 0 = rf = = 0.17 m µ g (0.75)(9.80 m/s 2 ) s _________________________________________________________________________________________ ____ REASONING The maximum torque will occur when the force is applied perpendicular to the diagonal of the square as shown. The lever arm l is half the length of the diagonal. From the Pythagorean theorem, the lever arm is, therefore, SSM WWW l= 1 2 0.40 m ( 0.40 m ) 2 + ( 0.40 m ) 2 = 0.28 m Since the lever arm is now known, we can use Equation 9.1 to obtain the desired result directly. 0.40 m 61. axis SOLUTION Equation 9.1 gives F τ = Fl = (15 N)(0.28 m) = 4.2 N ⋅ m _________________________________________________________________________________________ ___ 62. REASONING AND SOLUTION For a solid disk we know I = (1/2)MR2 so M = 2I/R2. Newton's second law for rotation yields I = (Στ)/α, so M = 2(Στ)/(αR2). α = (ω − ωo)/t = (−3.49 rad/s)/(15.0 s) = −0.233 rad/s2, so that Chapter 9 Problems M = ( − 2 −6.20 × 10 3 N ⋅ m ) ( −0.233 rad/s 2 )( 0.150 m ) 2 351 = 2.37 kg _________________________________________________________________________________________ ____ 163. REASONING AND SOLUTION the forces must be zero: The sum of F ΣFy = FW + FC – mg = 0 F W Therefore, 1.40 m FW + FC = mg C 0.60 m mg = (71.0 kg)(9.80 m/s2) = 696 N The sum of the torques must also be zero. Taking the axis for torques at the point just below the boulder, we have Στ = FC (0.60 m) – FW (1.40 m) = 0. a. Substituting for FW yields FC(0.60 m) – (696 – FC)(1.40 m) = 0 Solving for FC gives FC = 487 N b. Also, FW = 696 N – FC = . 209 N _________________________________________________________________________________________ ____ 64. REASONING AND SOLUTION Use conservation of angular momentum, Ioωo = (Io + I) ω, where Io = 1.2 × 10–3 kg⋅m2 and ωo = 0.40 rad/s The moment of inertia of the bug is I = mL2 = (5.0 × 10–3 kg)(0.20 m) 2 = 2.0 × 10–4 kg⋅m2 The final angular velocity is ω = Ioωo/(Io + I) = 0.34 rad/s 352 ROTATIONAL DYNAMICS _________________________________________________________________________________________ ____ 65. REASONING AND SOLUTION a. The rim of the bicycle wheel can be treated as a hoop. Using the expression given in Table 9.1 in the text, we have SSM Ihoop = MR 2 2 = (1.20 kg)(0.330 m) = 0.131 kg ⋅ m 2 b. Any one of the spokes may be treated as a long, thin rod that can rotate about one end. The expression in Table 9.1 gives Irod = 1 3 2 1 ML = 3 (0.010 kg)(0.330 m) 2 = 3.6 × 10 –4 kg ⋅ m 2 c. The total moment of inertia of the bicycle wheel is the sum of the moments of inertia of each constituent part. Therefore, we have I = Ihoop + 50 I rod = 0.131 kg ⋅ m 2 + 50(3.6 × 10 – 4 kg ⋅ m 2 ) = 0.149 kg ⋅ m 2 _________________________________________________________________________________________ ____ 66. REASONING AND SOLUTION The net torque about an axis through the elbow joint is Στ = (111 N)(0.300 m) − (22.0 N)(0.150 m) − (0.0250 m)M = 0 or 3 M = 1.20 × 10 N _________________________________________________________________________________________ ____ 67. REASONING The drawing shows the forces acting on the board, which has a length L. The ground exerts the vertical normal force V on the lower end of the board. The maximum force of static friction has a magnitude of µs V and acts horizontally on the lower end of the board. The weight W acts downward at the board's center. The vertical wall applies a force P to the upper end of the board, this force being perpendicular to the wall since the wall is smooth (i.e., there is no friction along the wall). We take upward and to the right as our positive directions. Then, since the horizontal forces balance to zero, we have µs V – P = 0 SSM P V θ W µs V (1) The vertical forces also balance to zero giving V – W = 0 (2) Chapter 9 Problems 353 Using an axis through the lower end of the board, we express the fact that the torques balance to zero as L PL sin θ − W cos θ = 0 (3) 2 F I G H JK Equations (1), (2), and (3) may then be combined to yield an expression for θ. SOLUTION Rearranging Equation (3) gives tan θ = W 2P (4) But, P = µs V according to Equation (1), and W = V according to Equation (2). Substituting these results into Equation (4) gives V 1 tan θ = = 2 µsV 2 µs Therefore, 1 1 θ = tan −1 = tan − 1 = 37.6° 2 µs 2 ( 0.650) F I G H JK L M N O P Q _________________________________________________________________________________________ ____ 68. REASONING AND SOLUTION a. The net torque about an axis through the point of contact between the floor and her shoes is Στ = − (5.00 × 102 N)(1.10 m)sin 30.0° + FN(cos 30.0°)(1.50 m) = 0 FN = 212 N b. Newton's second law applied in the horizontal direction gives Fh − FN = 0, so Fh = 212 N c. Newton's second law in the vertical direction gives Fv − W = 0, so Fv = 5.00 × 10 2 N _________________________________________________________________________________________ ____ 69. REASONING AND SOLUTION Since the change occurs without the aid of external torques, the angular momentum of the system is conserved: Ifωf = I0ω0. Solving for ωf gives I ωf = ω0 0 If ROTATIONAL DYNAMICS 354 where for a rod of mass M and length L, I 0 = 1 12 ML 2 . To determine If, we will treat the arms of the "u" as point masses with mass M/4 a distance L/4 from the rotation axis. Thus, 1 M L 2 M L 2 1 2 I f = + 2 = ML 12 2 2 4 4 24 and 1 2 12 ML ωf = ω0 = (7.0 rad/s)(2) = 14 rad/s 1 2 ML 24 _________________________________________________________________________________________ ____ 70. REASONING AND SOLUTION The conservation of energy gives (1/2) Iω2 = mg[(1/2) L]. Now the tip of the rod has, as it hits the ground, a speed of v = Lω, so ω = v/L. The moment of inertia of the rod is given by I = (1/3) mL2. Substituting the last two equations into the first equation and simplifying yields v= c 3gL = 3 9.8 m / s 2 hb2.00 mg= 7.67 m / s _________________________________________________________________________________________ ____ 71. REASONING AND SOLUTION Consider the left board, which has a length L and a weight of (356 N)/2 = 178 N. Let Fv be the upward normal force exerted by the ground on the board. This force balances the weight, so Fv = 178 N. Let fs be the force of static friction, which acts horizontally on the end of the board in contact with the ground. fs points to the right. Since the board is in equilibrium, the net torque acting on the board through any axis must be zero. Measuring the torques with respect to an axis through the apex of the triangle formed by the boards, we have SSM WWW L + (178 N)(sin 30.0°) + f s(L cos 30.0°) – Fv (L sin 30.0°) = 0 2 or 44.5 N + fs cos 30 .0 ° – FV sin 30.0 ° = 0 so that fs = (178 N)(sin 30.0 °) – 44.5 N cos 30.0 ° = 51.4 N _________________________________________________________________________________________ ____ 72. REASONING AND SOLUTION Newton's law applied to the 11.0-kg object gives Chapter 9 Problems T2 − (11.0 kg)(9.80 m/s2) = (11.0 kg)(4.90 m/s2) or 355 T2 = 162 N A similar treatment for the 44.0-kg object yields T1 − (44.0 kg)(9.80 m/s2) = (44.0 kg)(−4.90 m/s2) or T1 = 216 N For an axis about the center of the pulley T2r − T1r = I(−α) = (1/2) Mr2 (−a/r) Solving for the mass M we obtain M = (−2/a)(T2 − T1) = [−2/(4.90 m/s2)](162 N − 216 N) = 22.0 kg __________________________________________________________________________________________ ___ 73. CONCEPT QUESTIONS a. The magnitude of a torque is the magnitude of the force times the lever arm of the force, according to Equation 9.1. The lever arm is the perpendicular distance between the line of action of the force and the axis. For the force at corner B, the lever arm is half the length of the short side of the rectangle. For the force at corner D, the lever arm is half the length of the long side of the rectangle. Therefore, the lever arm for the force at corner D is greater. Since the magnitudes of the two forces are the same, this means that the force at corner D creates the greater torque. b. As we have seen, the torque at corner D (clockwise) has a greater magnitude than the torque at corner B (counterclockwise). Therefore, the net torque from these two contributions is clockwise. This means that the force at corner A must produce a counterclockwise torque, if the net torque produced by the three forces is to be zero. The force at corner A, then, must point toward corner B. SOLUTION Let L be the length of the short side of the rectangle, so that the length of the long side is 2L. We can use Equation 9.1 for the magnitude of each torque. Remembering that counterclockwise torques are positive and that the torque at corner A is counterclockwise, we can write the zero net torque as follows: Στ = FA l A + FB l B − FD l D = 0 b gc L h− b12 N gL = 0 FA L + 12 N 1 2 The length L can be eliminated algebraically from this result, which can then be solved for FA : b gch+ b12 N g= FA = − 12 N 1 2 6.0 N (pointing toward corner B) 356 ROTATIONAL DYNAMICS __________________________________________________________________________________________ ___ 74. CONCEPT QUESTIONS a. In the left design, both the 60.0 and the 525-N forces create clockwise torques with respect to the rotational axis at the point where the tire contacts the ground. In the right design, only the 60.0-N force creates a torque, because the line of action of the 525-N force passes through the axis. Thus, the total torque from the two forces is greater for the left design. b. The man is supporting the wheelbarrow in equilibrium. Therefore, his force must create a torque that balances the total torque from the other two forces. To do this, his torque must be counterclockwise and have the same magnitude as the total torque from the other two forces. Since the two forces create more torque in the left design, the magnitude of the man’s torque must be greater for that design. c. The magnitude of a torque is the magnitude of the force times the lever arm of the force, according to Equation 9.1. The drawing shows that the lever arms of the man’s forces in the two designs is the same (1.300 m). Thus, to create the greater torque necessitated by the left design, the man must apply a greater force for that design. SOLUTION The lever arms for the forces can be obtained from the distances shown in the drawing for each design. We can use Equation 9.1 for the magnitude of each torque. Remembering that counterclockwise torques are positive, we can write an expression for the zero net torque for each design. These expressions can be solved for the man’s force F in each case: Left design b gb g b gb g b b525 N gb0.400 mg+ b60.0 N gb0.600 mg= 189 N F= g Σ τ = − 525 N 0. 400 m − 60.0 N 0. 600 m + F 1.300 m = 0 1. 300 m Right design b gb g b b60.0 N gb0 .600 m g= 27.7 N F= g Σ τ = − 60.0 N 0.600 m + F 1. 300 m = 0 1.300 m __________________________________________________________________________________________ ___ 75. CONCEPT QUESTIONS a. The forces in part b of the drawing cannot keep the beam in equilibrium (no acceleration), because neither V nor W, both being vertical, can balance the horizontal component of P. This unbalanced component would accelerate the beam to the right. b. The forces in part c of the drawing cannot keep the beam in equilibrium (no acceleration). To see why, consider a rotational axis perpendicular to the plane of the paper and passing through the pin. Neither P nor H create torques relative to this axis, because their lines of action pass directly through it. However, W does create a torque, which is unbalanced. This torque would cause the beam to have a counterclockwise angular acceleration. Chapter 9 Problems 357 c. The forces in part d are sufficient to eliminate the accelerations discussed above, so they can keep the beam in equilibrium. SOLUTION Assuming that upward and to the right are the positive directions, we obtain the following expressions by setting the sum of the vertical and the sum of the horizontal forces equal to zero: Horizontal forces P cosθ − H = 0 ( 1) Vertical forces P sinθ + V − W = 0 ( 2) Using a rotational axis perpendicular to the plane of the paper and passing through the pin and remembering that counterclockwise torques are positive, we also set the sum of the torques equal to zero. In doing so, we use L to denote the length of the beam and note that the lever arms for W and V are L/2 and L, respectively. The forces P and H create no torques relative to this axis, because their lines of action pass directly through it. Torques W c L h− VL = 0 1 2 (3 ) Since L can be eliminated algebraically, Equation (3) may be solved immediately for V: V = 12 W = 1 2 b340 N g= 170 N Substituting this result into Equation (2) gives P sinθ + 12 W − W = 0 P= W 340 N = = 270 N 2 sinθ 2 sin39 ° Substituting this result into Equation (1) gives W I F G H2 sinθ JKcos θ − H = 0 H= W 340 N = = 210 N 2 tanθ 2 tan 39 ° __________________________________________________________________________________________ ___ 76. CONCEPT QUESTIONS a. Equation 8.7 from the equations of rotational kinematics indicates that the angular displacement θ is θ = ω0 t + 12 αt 2 , where ω0 is the initial angular velocity, t is the 358 ROTATIONAL DYNAMICS time, and α is the angular acceleration. Since both wheels start from rest, ω0 = 0 rad/s for each. Furthermore, each wheel makes the same number of revolutions in the same time, so θ and t are also the same for each. Therefore, the angular acceleration α must be the same for each. b. For the hoop, all of the mass is located at a distance from the axis equal to the radius. For the disk, some of the mass is located closer to the axis. According to Equation 9.6, the moment of inertia is greater when the mass is located farther from the axis. Therefore, the moment of inertia of the hoop is greater. Table 9.1 indicates that the moment of inertia of a hoop is I hoop = MR 2 , while the moment of inertia of a disk is I disk = 1 2 MR 2 . c. Newton’s second law for rotational motion indicates that the net external torque is equal to the moment of inertia times the angular acceleration. Both disks have the same angular acceleration, but the moment of inertia of the hoop is greater. Thus, the net external torque must be greater for the hoop. SOLUTION Using Equation 8.7, we can express the angular acceleration as follows: θ = ω0 t + 12 αt 2 or α= c 2 θ − ω0 t t h 2 This expression for the acceleration can now be used in Newton’s second law for rotational motion. Accordingly, the net external torque is L2 cθ − ω t hO M t P M P N Q L2 b13 rad g− 2 b0 rad / sgb8 .0 sgO =b 4 .0 kg g P= 0.20 N ⋅ m b0.35 mg M M 8 . 0 s P b g N Q L2 cθ − ω t hO Στ = I α = MR M P t M P N Q L2 b13 rad g− 2 b0 rad / sgb8 .0 sgO = b 4 .0 kg g P= 0.10 N ⋅ m b0.35 mg M M 8 . 0 s P b g N Q Hoop Στ = I hoop α = MR 2 0 2 2 2 Disk disk 1 2 1 2 0 2 2 2 2 __________________________________________________________________________________________ ___ 77. CONCEPT QUESTIONS a. According to Equation 9.6, the moment of inertia for rod A is just that of the attached particle, since the rod itself is massless. For rod A with its attached particle, then, the moment of inertia is I A = ML2 . According to Table 9.1, the moment of inertia for rod B is I B = 13 ML2 . The moment of inertia for rod A with its attached particle is greater. Chapter 9 Problems 359 b. Since the moment of inertia for rod A is greater, its kinetic energy is also greater, according to Equation 9.9 KE R = 12 Iω2 . SOLUTION Using Equation 9.9 to calculate the kinetic energy, we find Rod A = Rod B cML hω b0.66 kg gb0 .75 mgb4 .2 rad / sg = 3.3 J c ML hω b0 .66 kg gb0. 75 mgb4 .2 rad / sg = 1.1 J KE R = 12 I A ω2 = 1 2 1 6 2 2 2 KE R = 12 I Bω2 = = 1 2 1 2 1 3 2 2 2 2 2 __________________________________________________________________________________________ ___ 78. CONCEPT QUESTIONS a. The force is applied to the person in the counterclockwise direction by the bar that he grabs when climbing aboard. b. According to Newton’s action-reaction law, the person must apply a force of equal magnitude and opposite direction to the bar and the carousel. This force acts on the carousel in the clockwise direction and, therefore, creates a clockwise torque. c. Since the carousel is moving counterclockwise, the clockwise torque applied to it when the person climbs aboard decreases its angular speed. SOLUTION We consider a system consisting of the person and the carousel. Since the carousel rotates on frictionless bearings, no net external torque acts on this system. Therefore, angular momentum is conserved, and we can set the total angular momentum of the system before the person hops on equal to the total angular momentum afterwards. Afterwards, the angular momentum includes a contribution from the person. According to Equation 9.6, his moment of inertia is I person = MR 2 , since he is at the outer edge of the carousel. I carousel ωf + I person ωf 144424443 = I carousel ω0 1424 3 Initial total angular momentum Final total angular mo mentum ωf = I carousel ω0 I carousel + I person = I carousel ω0 I carousel + MR 2 c125 kg ⋅ m hb3.14 rad / sg = = 125 kg ⋅ m + b 40. 0 kg g b1.50 m g 2 2 2 1.83 rad / s 360 ROTATIONAL DYNAMICS __________________________________________________________________________________________ ___