Figure B6 Measured and calculated natural frequencies for an inclined, slack Double Armor Steel 

 (DAS) cable. 



Figure B7 The geometry and nomenclature for an inclined slack cable of length L and mass per unit 

 length m. 



Figure B8 Numerical results for the lowest two in-plane modes of an inclined slack cable. 



Figure CI Measured natural frequencies for the Double-Armored Steel (DAS) cable mounted in the 

 DTNSRDC test apparatus. 



Figure C2 Measured natural frequencies for the Uniline cable mounted in the DTNSRDC test ap- 

 paratus. 



Figure C3 The measured in-air (structural) log decrements 5 of the Uniline cable in the DTNSRDC 

 test apparatus. 



Figure C4 The measured in-air (structural) log decrements 8 of the DAS cable in the DTNSRDC test 

 apparatus. 



Figure C5 Added mass coefficient Q^ plotted against vibration Reynolds number Re^,. 



Figure C6 Reduced damping k^ plotted vibration Reynolds number Re„. 



Figure C7 A comparison of the computed natural frequencies of the Double Armor Steel (DAS) cable 

 with measured frequencies. 



Figure Dl Wake-oscillator prediction of the cross flow vortex-excited response of a circular cylinder. 



Figure El Predicted cross flow displacement amplitude Y/D plotted against the reduced damping 



l-nl^Jy. for the sine mode resonant response of a flexible structure. 



Figure E2 Computed evolution with time of the vortex shedding in the wake of an oscillating cylinder. 



