Page 500 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
P. 500

470                SLENDER STRUCTURES AND AXIAL FLOW

                     Benjamin (1963) recognized this and so considered next a system which is unbounded
                   in the flow direction, x, and which is disturbed by  a  sinusoidal wave travelling in  that
                   direction - see also  Ye0  & Dowling  (1987). The  motion  within  an  interval of  x  may
                   be considered to comprise two modes q = qI(t) sin ax and  q = q2(t) cos ax, in  which
                   q1  and q2  are oscillations in  quadrature. Through the  action of  the  flow there may  be
                   coupling between these two modes, and so q is generally taken to be  complex, on the
                   understanding that  %e(q exp(iax)) describes the  physical disturbance. The equation of
                   motion is  still of  the form of  (C.l), but  now we insist that M  < 0, so that m - M  > 0
                    always; k and K  are real, but C can now be complex, C = C,. + ici (cf. the Coriolis term
                    in the pipe problem).
                      Corresponding to  (C.2),  the  energy transfer  W  averaged over x is  given by  the  real
                    part of the integral of  kpq, where p is the complex conjugate of  Q. The term icq in
                    Q makes no contribution to W, and so the expressions for % and E  in (C.4)-(C.6)  are as
                    before, except that C is now replaced by  C,.  Thus, dE/dt takes the sign of  C,. - c.
                      Representing the solutions of  (C.l) by q exp(-ivt),  where v  is complex, we get

                                                                       2i(c - Cr)
                                V=                                                       ((2.7)
                                   2(m - M)           c,

                    where R = [4(m - M)(k - K) + (c - Cr)’]/G2. It is recognized that instability is  indi-
                    cated by 4m(v) > 0, where
                                        r                                              1  I?-










                    Since m - M  > 0, R may be positive or negative, depending on whether k  > K  or other-
                    wise. The following three cases may be distinguished. (a) When R  > 0, 4m(v) > 0 for
                    both solutions if  C,. > c,  which from (C.6) corresponds to dE/dt > 0 and hence to class
                    B instability, i.e. to case (i) in the foregoing. (b) When -1  < R < 0, one solution is again
                    of  class B, but  the  other one  is  of  class A, being  unstable for  c > C,..  (c) The case of
                    R < -1  corresponds to class C instability, not considered here. Therefore, it is clear that
                    for -1  < R < 0 and c > C,. the physical system obeys the arguments given in (ii) in the
                    foregoing and is thus destabilized by  damping.
   495   496   497   498   499   500   501   502   503   504   505