Interestingly, from my analysis at the time, it seems a major factor in the carnage, apart from the weather itself, was that this was the first real test of the widespread use of carbon fibre in yachting.
What many of the designers apparently failed to fully appreciate is that the advantage of carbon fibre is not that it is stronger than glass,but that it is a lot stiffer. This means that where glass reinforcement, being elastic, allows stresses to spread, enabling you to get away with structures that have built in stress concentrations. But if you do this with carbon fibre, it will not spread, and you will get failure at the stress concentration. This is why you have things like a yacht where the backstay pulled out the entire transom, but it also seems to be behind many other failures.
Designers and builders (and possibly scrutineers) have apparently learned from this, and we don't seem to have had a repeat.
What many people do not appreciate (but designers should) is that for almost any structure, the overall strength/mass ratio of the structure is dependent not on the strength of the material, but its elasticity or stiffness, measured by Young's modulus - some parts depend on tensile strength, but that is the easy bit. And in structures on boat in rough seas, most loads are alternately compression and tension.
The reason for this is that failure of compressional structural members for almost any realistic structure will almost always be due to what is called Euler buckling. And the only material property involved in calculating this strength is Youngs modulus.
An interesting feature of most realistic materials for building things like cars, planes, boats is that the ratio of density to Youngs Modulus is almost identical. Almost the only exception to this is carbon fibre reinforced plastic, which is a lot stiffer than would be expected from its density. This means you can make panels for example thinner and hence lighter for the same strength, but where building in fibreglass you could assume that if it is strong enough in compression it is plenty strong enough in tension, the same may not necessarily be the case in tension, especially if you do not properly manage stress concentrations. This explains the transom failure mentioned above, but also some of the mast failures etc.


 
					
					 
				
				
				
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					 Originally Posted by NavyDiver
 Originally Posted by NavyDiver
					
 
						
					 
						
					 
						
					 
						
					
 
			
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