Page 215 - Intro to Tensor Calculus
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                               GMm
                         ~
                                    ~ denote the inverse square law force of attraction between the earth and sun, with
              I 25. Let F = −       r
                                 r 3
               G a universal constant, M the mass of the sun, m the mass of the earth and  ~ r  a unit vector from origin
                                                                                     r
               at the center of the sun pointing toward the earth. (a) Write down Newton’s second law, in both vector
                                                                                             d
                                                                                                        ~
                                                                                                r
               and tensor form, which describes the motion of the earth about the sun. (b) Show that  (~ × ~v)= 0and
                                                                                             dt
                                          ~
                                  r
                           r
               consequently ~ × ~v = ~ ×  d~ r  = h =aconstant.
                                      dt
              I 26. Construct a set of axes fixed and attached to an airplane. Let the x axis be a longitudinal axis running
               from the rear to the front of the plane along its center line. Let the y axis run between the wing tips and
               let the z axis form a right-handed system of coordinates. The y axis is called a lateral axis and the z axis is
               called a normal axis. Define pitch as any angular motion about the lateral axis. Define roll as any angular
               motion about the longitudinal axis. Define yaw as any angular motion about the normal axis. Consider two
               sets of axes. One set is the x, y, z axes attached to and moving with the aircraft. The other set of axes is
               denoted X, Y, Z and is fixed in space ( an inertial set of axes). Describe the pitch, roll and yaw of an aircraft
               with respect to the inertial set of axes. Show the transformation is orthogonal. Hint: Consider pitch with

               respect to the fixed axes, then consider roll with respect to the pitch axes and finally consider yaw with
               respect to the roll axes. This produces three separate transformation matrices which can then be combined
               to describe the motions of pitch, roll and yaw of an aircraft.

                                                            3
                                                         2
                                                      1
                                                                                        i
                                                                                            i
              I 27. In Cartesian coordinates let F i = F i (x ,x ,x ) denote a force field and let x = x (t) denote a curve
                                                                                          !
                                                                                      i    2                i
                                                                           d   1    dx            1  2  3  dx
               C. (a) Show Newton’s second law implies that along the curve C   m           = F i (x ,x ,x )
                                                                           dt  2     dt                   dt
               (no summation on i) and hence
                           "                                !#
                                     1    2     2    2     3    2                  1       2       3
                         d  1      dx        dx       dx          d  1   2      dx       dx      dx
                              m          +         +           =       mv   = F 1   + F 2   + F 3
                         dt  2      dt       dt        dt         dt 2           dt      dt      dt
                                                                 i
                                                                                   i
               (b) Consider two points on the curve C,say point A, x (t A ) and point B, x (t B ) and show that the work
               done in moving from A to B in the force field F i is
                                                    t B  Z  B
                                             1   2             1       2       3
                                              mv      =    F i dx + F 2 dx + F 3 dx
                                             2           A
                                                   t A
               where the right hand side is a line integral along the path C from A to B. (c) Show that if the force field is
                                                     2
                                                  1
                                                        3
               derivable from a potential function U(x ,x ,x ) by taking the gradient, then the work done is independent
               of the path C and depends only upon the end points A and B.
              I 28. Find the Lagrangian equations of motion of a spherical pendulum which consists of a bob of mass m
               suspended at the end of a wire of length `, which is free to swing in any direction subject to the constraint
               that the wire length is constant. Neglect the weight of the wire and show that for the wire attached to the
               origin of a right handed x, y, z coordinate system, with the z axis downward, φ the angle between the wire
               and the z axis and θ the angle of rotation of the bob from the y axis, that there results the equations of
                                                       2          2
                           d     2  dθ                d φ     dθ              g
               motion         sin φ     =0     and        −        sin φ cos φ +  sin φ =0
                          dt        dt                 dt 2   dt              `
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