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- Jul 8, 2011
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Someone is giving themselves way too much credit, after several days of being spoon fed .......... :lol: and continues to confuse with a simple chart.
pommie john said:hobot said:The chart must only show basic concept as not that close to reality. For instance it shows with .7 CoD it takes 50 hp to do the ton but we know we can sit bolt upright on about any C'do at 100 with less than 50 rwhp. CoD relates more to shape than frontal area so a dropped brick might hit the ground before a dropped faired cycle and rider. Also calculations of this sort are same fuzzy logic as engine power calculators.
From a quick glance that chart shows CoD per Square metre ( of frontal area)
I imagine that you have to take into account the frontal area and apply that to the graph.
Dances with Shrapnel said:Someone is giving themselves way too much credit, after several days of being spoon fed .......... :lol: and continues to confuse with a simple chart.
acotrel said:A friend of mine was a senior research scientist at Aeronautical Research Labs in Melbourne and ran the transonic wind tunnel. Everything was done with models in a tube which narrowed down to give the velocity. Monitoring was done with pressure sensors. I think most incorporated pitot tubes.
Rohan said:Someone here was quoting dinosaur numbers.
And didn't know it /even denied it until repeatedly prompted !!
Dances with Shrapnel said:Drag coefficient I referred to is from Phil Irving's book and probably some obscure imperial based unit, something like 0.0008. If you have his book, look it up. I am on the road so cannot help you in your quest.
Rohan said:If someone reworks the aero so the drag coefficient goes from .40 to .30, and "0.0001 improvement yields a 12.5% reduction in drag",
does that mean they get a 12500 % decrease in drag ???
Rohan said:The penny has finally dropped.
You are using all imperial figures.
The coefficient of drag is different in imperial ??
acotrel said:A simple question about what system of units was being used in the discussion might have helped ? .
Rohan said:acotrel said:And Mr dws initially refuted the metric values.
Rohan said:Wasn't it you that quoted 'Motorcycle Engineering'
Rohan said:It appears you have gone back and re-edited a number of your posts.
And P224 takes me nowhere in anything I own or have read. (Clymer versions - criticism noted).
So its tough to see where we diverged.
Dances with Shrapnel said:Using your more common units of coefficient, reducing the coefficienct from say 4.0 to 3.5 yields a 12.5% reduction in drag.
Dances with Shrapnel said:Using your more common units of coefficient, reducing the coefficienct from say .40 to .35 yields a 12.5% reduction in drag. Phil Irving presented a coeeficient of 0.0008 and I arbitrarily picked 0.0007 (net 0.0001) which yields the same percentage reduction. I have a hunch Irving may have combined a few terms; don't know for sure without digging into an old fluid dynamics text and studying it a bit.
So design or redesign a complete bike for 2" lower and maybe 5-8% reduction in drag or reduce the coefficient by 10-12 or more percentage points. It could be be as easy as adopting a different tuck in riding position or a modified tail piece.
Irving was pragmatic. Testing to measure results could/would be done on a flat out and read the tach.
acotrel said:I'm glad he has found a new friend to irritate. Do you live anywhere near him ? For God's sake take him to a race circuit and let him ride a real motorcycle. So far everything about him has been interpreted supposition.