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               likely to suffer stronger periodic excitation than the originating body. This commonly arises
               where a power station, for example, is served by two or more chimneys. Clearly this only
               operates when the wind is within a small range of direction, but extends to separations as
               large as 15 times the diameter. The most unfavourable effects occur when the chimneys are
               identical, as resonant motion of the upwind element leading to enhanced regularity of the
               vortex street will coincide with resonance of the affected downwind element. For this case it
               has been suggested that response of the downwind element may be twice that predicted for an
               isolated stack if the separation is 5D, or 1.5 times the isolated value if the separation is 10D
               (Vickery, 1981; see also informative annex C.3.2.3 of the Eurocode ENV 1991–2–4).
                 Serious consideration must be given to this problem when slender modern structures are
               located in proximity to existing structures causing greater disturbance to the flow. The effect
               may be to present a significantly organized vortex street, changing with increasing separation
               to greater resemblance of a normal turbulence field but with strongly enhanced strength in the
               range of frequencies likely to embrace the structural resonant frequency. The term ‘buffeting’
               has been expressly applied to this effect in UK usage, in distinction from its application to
               turbulence effects in general in the aeronautical field and elsewhere. The seminal example
               was the decision to build a stiff lattice arch bridge in place of the proposed suspension bridge
               over the Mersey at Runcom, in proximity to the nineteenth century through truss railway
               bridge (Scruton et al., 1955; Grillaud et al., 1992; Bietry et al., 1994).
                 Two other resonant potential responses to vortex shedding should be borne in mind,
               although generally out of range or readily circumvented when the excitation derives from the
               natural wind. There is a weak in-line excitation, with one cycle for each vortex shed, giving
               resonance at one-half of the cross-flow resonance windspeed. The Scruton number limit to
               effectively avoid a structural problem is perhaps K =7. This has been observed with wind
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               excitation only in exceptional circumstances such as aluminium tubular members in a frame
               with very low damping, but can be a serious problem in water (e.g. for pile columns
               supporting a jetty). The second phenomenon possible at this reduced velocity is excitation of
               the ovalling mode of the structural section, which should be circumvented by ensuring a
               sufficiently high frequency, by stiffening if necessary, so that resonance is out of the practical
               windspeed range.


                              3.2.7 Vortex shedding: design rules for circular sections

               The windspeed corresponding to resonance at the Strouhal frequency for a stationary structure
               can be robustly estimated, and if this exceeds the practical windspeed for the site, no further
               action is required. If not (as is commonly the case), the stresses caused by resonant response
               must be checked. Lock on may lead to a slightly greater response at a windspeed perhaps 20
               per cent greater than the basic Strouhal resonance; for transcritical Reynolds number (nD 2
               significantly
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