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552  Elementary aeroelasticity







                                                             ass m

                                                L--J  -l
                                               I ‘-1  -





                  Fig. 13.7  Oscillation of a masdspring system.   X

                  an aircraft is a complex process since such a structure possesses an infinite number of
                  natural  or normal  modes of  vibration.  Simplifying assumptions, such as breaking
                  down the structure into a number of concentrated masses connected by weightless
                  elastic beams (lumped mass concept) are made, but whatever method is employed
                  the  natural  modes  and frequencies of  vibration  of  the  structure must  be  known
                  before  flutter  speeds and  frequencies can  be  found.  We  shall discuss flutter and
                  other dynamic aeroelastic phenomena later in the chapter; for the moment we shall
                  consider methods  of  calculating normal modes and  frequencies of  vibration of  a
                  variety of beam and mass systems.
                    Let us suppose that the simple mass/spring system shown in Fig. 13.7 is displaced
                  by a small amount xo and suddenly released. The equation of the resulting motion in
                  the absence of damping forces is
                                                mx+kx=O                             ( 13.36)

                  where k is the spring stiffness. We see from Eq. (13.36) that the mass, m, oscillates with
                  simple harmonic motion given by

                                              x  = xo sin(wt + E)                   (13.37)
                  in which 3 = k/m and E  is a phase angle. The frequency of the oscillation is w/2~
                  cycles per second and its amplitude xo. Further, the periodic time of the motion,
                  that is the time taken by one complete oscillation, is ~K/w. Both the frequency and
                  periodic  time  are  seen  to  depend  upon  the  basic  physical  characteristics of  the
                  system,  namely  the  spring  stiffness  and  the  magnitude  of  the  mass.  Therefore,
                  although the  amplitude of  the  oscillation may  be  changed by  altering the  size of
                  the initial disturbance, its frequency is ked. This frequency is the normal or natural
                  frequency of the system and the vertical simple harmonic motion of the mass is its
                  normal mode of vibration.
                    Consider now the system of n masses connected by  (n - 1) springs, as shown in
                  Fig.  13.8. If  we  specify that  motion  may  only  take  place in  the direction of  the
                  spring axes then the system has n degrees of freedom. It is therefore possible to set
                  the system oscillating with simple harmonic motion in n different ways. In each of
                  these  n modes  of  vibration  the  masses  oscillate in  phase  so  that  they  all attain
                  maximum  amplitude at the  same time  and  pass  through their zero displacement
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