Fig. 1 Strouhal versus Reynolds number from Ref. [ 2 ] Strouhal versus Reynolds number from Ref. [2] More

Fig. 2 Strouhal versus Reynolds number from Ref. [ 8 ] Strouhal versus Reynolds number from Ref. [8] More

Fig. 3 Strouhal versus Reynolds Strouhal versus Reynolds More

Fig. 4 Strouhal versus Reynolds—Re < 2E + 3 Strouhal versus Reynolds—Re < 2E + 3 More

Fig. 5 Strouhal versus Reynolds—2E + < Re < 1E + 5 Strouhal versus Reynolds—2E + < Re < 1E + 5 More

Fig. 6 Strouhal versus Reynolds—Re > 1E + 5 Strouhal versus Reynolds—Re > 1E + 5 More

Fig. 7 VIV response data from rigid cylinders and flexible cylinders VIV response data from rigid cylinders and flexible cylinders More

Fig. 8 Varying effects of Strouhal number for smooth and rough cylinders Varying effects of Strouhal number for smooth and rough cylinders More

Fig. 9 Effects of turbulence ranging from 0.4% to 9.1%, derived from [ 27 ] Effects of turbulence ranging from 0.4% to 9.1%, derived from [27] More

Fig. 10 Test results and associated lines of best fit with average across test series, derived from Ref. [ 7 ] Test results and associated lines of best fit with average across test series, derived from Ref. [7] More

Fig. 11 Wind tunnel data testing Wind tunnel data testing More

Fig. 12 Frequency versus velocity from various testing programs [ 19 , 20 , 28 – 30 ] Frequency versus velocity from various testing programs [19,20,28–30] More

Fig. 1 Static configuration of the synthetic lazy wave riser configuration Static configuration of the synthetic lazy wave riser configuration More

Fig. 2 Summary of different results of Case 1 with A = 0.5 m, T = 7.5 s Summary of different results of Case 1 with A = 0.5 m, T = 7.5 s More

Fig. 3 Summary of different results of Case 2 with A = 3.5 m, T = 6.0 s Summary of different results of Case 2 with A = 3.5 m, T = 6.0 s More

Fig. 4 Standard deviation of CF VIV displacement responses Standard deviation of CF VIV displacement responses More

Fig. 5 Spectra analysis out-of-plane (CF) curvature of the SLWR Case 1: A = 0.5 m, T = 7.5 s Spectra analysis out-of-plane (CF) curvature of the SLWR Case 1: A = 0.5 m, T = 7.5 s More

Fig. 6 Spectra analysis out-of-plane (CF) curvature of the SLWR Case 2: A = 3.5 m, T = 6.0 s Spectra analysis out-of-plane (CF) curvature of the SLWR Case 2: A = 3.5 m, T = 6.0 s More