I have done wet flow testing, sonic testing, and always go back to individual runner testing before finalizing the averages. IF and I say IF the individual runner is optimized first, then opening up the manifold for all eight runners to flow through the one port, the flow will be nearly identical in flow. I have tested that on single plane intakes, dual plane intakes, 6V intakes, 8V intakes, and TW, TR, HR 4V, HR 8V, TP intakes, etc., and every time if the one port is properly blended in the plenum, shaped with taper, the individual flow will be the same as all eight open ports. BTDT too many times to argue any more about it. I have flow tested Wilson CNC'd $2500.00 intakes that folks were having problems with fuel distribution on, and found as much as 80 cfm difference between end ports and center ports. I always try to get the end ports on single plane intakes to match the flow of the center ports, and on dual plane intakes I try to get those within 5% of each ports flow. The RPM mentioned above has a difference of less than 9 cfm between ports in a dual plane manifold that flows 383.27 cfm. If that is not respectable, than I surrender to anyone who can do better. Signing off. Joe-JDC
I don't think anyone is arguing with you. It's just you're only addressing one piece of the issue. I clumsily asked a similar question quite a while back and though I got a lot of useful feedback I didn't get to the heart of the matter in the way folks are discussing it right now. Fuel distribution involves bringing a gas (air) and a liquid (gasoline) to the combustion chamber in equal, homogenous proportions.
It helps that gasoline is so volatile but it's density is significantly different than air so complete atomization of the fuel and homogenous mixing with air is difficult to achieve in every runner across the rpm range.
I found Jay's painstaking efforts on the SOHC dang interesting. I'm more concerned about balancing for engine longevity than I am about performance but I think it's all tied together.