Page 27 - SP015 Past Years PSPM Chapter 6 -14 Ver 2020
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PSPM SP015



                     PSPM 2015/2016  SF016/2  No. 5(b)

               45.  A 15 N m torque acts on a grinding wheel after the power is switched off. Given the
                                                                                                        2
                     angular  velocity  of  the  wheel  is  1200  rpm  and  its  moment  of  inertia  is  0.8  kg  m ,
                     calculate the time for the wheel to stop.                                      [3 m]



                     PSPM 2016/2017  SF016/2  No. 5(b)

                                                                 2
               46.  A  flywheel  with  moment  of  inertia  8  kg  m   is  acted  upon  by  a  constant  torque  of
                     50 N m. Calculate the

                     (a)  angular acceleration.                                                     [1 m]

                                                                -1
                     (b)  time for it to rotate from rest to 70 rad s .                             [1 m]

                                                                    -1
                     (c)  power when the angular velocity is 50 rad s .                             [1 m]



                     PSPM 2017/2018  SF016/2  No. 5(c)

               47.





                                           1.5 m




                                                                 F = 0.8 N

                                                   FIGURE 8.21

                     FIGURE 8.21 shows a 0.75 kg airplane model is attached by an arm rod of negligible
                     mass flies in horizontal circle 1.5 m in radius. The airplane model acts a force of 0.8 N
                     perpendicular to the rod. By assuming the airplane as a point mass, calculate the

                     (a)  torque about the axis passing through the centre of the circle.           [2 m]

                     (b)  angular acceleration of the airplane.                                     [2 m]

                     (c)  linear acceleration of the airplane tangent to its flight path.           [2 m]






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