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0593_C08_fm  Page 273  Monday, May 6, 2002  2:45 PM





                       Principles of Dynamics: Newton’s Laws and d’Alembert’s Principle            273


                       P8.5.2: Repeat Problem P8.5.1 for a tube radius r of 0.5 m, a particle mass m of 0.1 kg, and
                       a speed v relative to the tube of 1 m/sec.
                       P8.5.3: Repeat Problems P8.5.1 and P8.5.2 if the rotation rate Ω of the tube is increasing
                                 2
                                                                                            2
                       at 7 rad/sec  and the speed v of P relative to the tube is increasing at 10 ft/sec  for P8.5.1
                                  2
                       and 3 m/sec  for P8.5.2.
                       Section 8.7 Projectile Motion
                       P8.7.1: An object P is thrown vertically from the ground with a speed v . Using Eq. (8.7.11)
                                                                                     0
                                                                     2
                       show that the maximum height h reached by P is  v 2.
                                                                        g
                                                                     0
                       P8.7.2: See Problem P8.7.1. An object P is dropped from rest at a height h above the ground.
                       Show that the speed v at which P strikes the ground is  2 gh.
                       P8.7.3: See Problem P8.7.1. An object P is thrown vertically from the ground with a speed
                       of 15 ft/sec. Find the maximum height h reached by P.
                       P8.7.4: See Problem P8.7.2. An object P is dropped from rest from a height of 30 m. Find
                       the speed of impact of P with the ground.
                       P8.7.5: A projectile is launched from a horizontal surface at a speed v of 50 ft/sec at an
                       angle θ of 30° relative to the horizontal as in Figure P8.7.5. Determine the range d where
                       the projectile impacts the horizontal surface and the maximum height h reached by the
                       projectile.

                                                                   v = 50 ft/sec
                                                                               d
                                                                   θ    = 30°   h
                       FIGURE P8.7.5
                       A projectile launched on a horizontal plane.

                       P8.7.6: See Problem P8.7.5. Repeat Problem P8.7.5 for launch angles θ of (a) 35°, (b) 40°,
                       (c) 45°, (d) 50°, (e) 55°, and (f) 60°. Tabulate and graph the results for d and h as a function
                       of θ. Verify that the range d is a maximum for θ = 45°.
                       P8.7.7: See Problem P8.7.5. Repeat Problem P8.7.5 if the projectile is launched from a point
                       8 ft above the horizontal surface as in Figure P8.7.7.


                                                                                          T
                                                                           v = 80 ft/sec
                           v = 50 ft/sec
                              θ = 30°
                                      h
                           8 ft
                                                                            θ
                                        d                                P

                                                                     FIGURE P8.7.8
                       FIGURE P8.7.7                                 A projectile P launched toward a target T.
                       A projectile launched above a horizontal surface.

                       P8.7.8: A projectile P is launched at 80 ft/sec toward a target T which is 30 ft high and 40
                       ft away (measured horizontally) as in Figure P8.7.8. Determine the appropriate launch
                       angles θ.
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