Figure 2.10 Steady drag-induced deflection at the tip of a free-ended cantilever marine pile. 



Figure 2.11 Spanwise correlation coefficients pab for the velocity signals measured in the wake of a vi- 

 brating cable. 



Figure 2.12 Distribution of displacement amplitude Y/D, magnitude of the spanwise correlation 

 coefficient p.^g, and the spectral content of the vortex shedding at the vibration frequency /(C„) and at 

 the Strouhal frequency fsiC^). 



Figure 2.13 Spanwise correlation coefficient Rp between the fluctuating pressures measured on a vibrat- 

 ing pivoted rigid cylinder. 



Figure 2.14 Peak cross flow displacement amplitude Y/D (root-mean-square of Y) plotted against re- 

 duced velocity V^ for a flexibly-mounted circular cylinder. 



Figure 2.15 Inverse reduced velocity F^"' for maximum displacement amplitudes plotted against the 

 Reynolds number for roughened cylinders. 



Figure 2.16 Universal Strouhal number St* plotted against the wake Reynolds number Re*. 



Figure 2.17 The universal wake drag coefficient Co plotted against the wake Reynolds number. 



Figure 2.18 The cross flow induced displacement amplitude Y/D for flexible, yawed cylinders in uni- 

 form flow plotted against the reduced velocity V^. 



Figure 2.19 Lock-on boundaries (in terms of the cross flow displacement amplitude 2Y/D) plotted 

 against the ratio of vibration and Strouhal frequencies. 



Figure 2.20 Total unsteady transverse force coefficient at the locked-on vibration frequency, Ctmax-, 

 plotted against the reduced velocity K^. 



Figure 2.21 Total unsteady transverse force coefficient Cj-, measured on smooth and rough circular 

 cylinders vibrating in the cross flow direction plotted against the displacement amplitude 2 Y/D. 



