Page 48 - Fluid-Structure Interactions Slender Structure and Axial Flow (Volume 1)
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CONCEPTS, DEFINITIONS AND METHODS                    31




















               Figure 2.6  Typical  form  of  correlation  functions: R,](rI, 0) for  points  i  and  j  separated  by  a
               variable rl in the streamwise direction; and R,,(r2, 0) for points separated by rz in the cross-stream
                                      direction - following Tritton (1988).

                 The Fourier transform of  the autocorrelation function gives the frequency spectrum of
               the turbulence at a given point,

                                                  to
                                     fi,(u) =  /  R;,(r, r)ePiwr dr,                (2.89)
                                             2rc  --w

               where  w  is the radian frequency. The fij(w) give a measure of  the energy spectrum of
               the turbulence. Hence, a peak in the spectrum denotes a dominant frequency, which could
               excite  an  underlying  structure,  for  instance. The energy spectrum  is often  described  in
               terms  of  the  wavenumber  k, generally  a  3-D  vector, k = (kl, k2, k3IT, with  each  k; =
               1/2rcA;, A;  being the wavelength of turbulent fluctuations associated with a frequency w;.
               Thus, the equivalent of  (2.89) in terms of k is

                                                                                    (2.90)


               This may be expressed as a function of a scalar variable by averaging it over all directions
                                                 s
               of k; thus,
                                         @;j(k) =  4j (k) dA(k),                    (2.9 1 )

               where  k  = llkll,  and  the  integration  is  over  the  surface of  a  sphere  of  which  dA is  an
               element,  so that @;,(k) is the contribution to the energy tensor uiuj from wavenumbers
               whose magnitudes lie between k  and k + dk  (Batchelor 1960, Chapter 111).
                 Another quantity of  interest is the turbulence intensity, which may be defined by

                                                      112
                                             TU= ($K)  /U                           (2.92)
               for sensibly one-dimensional flow, where
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