by 1bolt » Sun Jan 25, 2009 12:31 am
Randy I don't know so I'll let someone else field that.
I did want to add that since my last post on this subject I've been playing with Engine Analyzer Pro more. EApro uses Flow coefficients, not the square root approximation.
The square root formula is only a good predictor of flow through a square or sharp edge orifice. The flow coefficient of either is usually around .62 right? Well a good port especially at low lifts can be close to .80 (a valve with the same opening as a sharp orifice is going to be considerably more efficient much like a nozzle is) and at higher lifts can often be lower around the .5 range
Not only do ports not behave like a sharp edge orifice which is what the square root forumla is supposed to approximate (it's a model), they are usually considerably better or worse depending on lift and how well done the porting work was.
If you're using that formula, for example; to convert CFM at one lift/depression to another, then you will be applying a model that assumes .62 Cd at all lifts when in fact they are likely to be considerably better or worse on each end of the valve lift range. Thus your CFM conversion is okay looking in the middle lift ranges. And that is why you can see differences (sometimes big ones like earlier in this thread) they are magnified at low and high lift as the Cd of the port gets further and further away from the .62 assumption of the Square root formula.
CFM isn't the only thing we could be measuring. One way to look for differences at the same lift with more or less depression (or floating depression) would be velocity maping. I haven't done it myself but I'd be curious to map velocities (looking for relative differences between areas of the port) with higher and lower depression.
Simon