scjoe
Contributor
This topic has proceeded as it always does. If the OP is still following the thread, he might want to Google Dave Pendergast. He did two different studies on fins that are worth reading and understanding.
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Since that split fins; specifically Atomic Aquatics split fins, have been tested by ScubaLab to show that they have pretty much the same thrust and speed as a very good solid fins, so yeah, I think that my fins will do just fine with doubles and drysuit.
If you made a couple more cuts (probably not as deep), you'd have a "spork". Some (campers?) find them quite useful.
If you CAN'T see any advantages to using a split fin design, maybe this image of a dolphin's tail could help:
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BTW, I don't think their "split-fins" have any more trouble with current than mine do.
Please not that there ARE some split-fins that don't do well in current. I returned a pair of split-fins that I found inadequate/too flimsy for even single-tank recreational diving. As I mentioned in an earlier post to this thread, not all (split)fins are created equal.
I'm also generally not trying to move a truck-load of gear through the water when I go diving.
Just my opinion.
Cheers.
These are the fins I use, I find that I can get 15 PSI to the furlong improvement with these fins over any other fin out there. They have the awesomeness of paddles, with multiple splits to be even MORE efficient than a lowly single split.
I am quite sure the Scubalab test was conducted utilizing a single tank configuration...
Pullmyfinger, your comparison is utter nonsense. Spoon is designed to hold liquid. Fins are designed to move liquid. You don't push fin perpendicular to where you go but at certain angle. Fins should be pushing water in certain direction based on their design.
Airplane wing is not split and provides decent lift. However if you observe an eagle wing you will see certain small splits at the end of weathers. How much you want to bet that eagle wing is more efficient in providing lift than airplane wing? If we had better way of imitating eagle wing on an airplane I am sure we could improve the efficiency and design.