U-flow horsepower limitations

Is this with or without epoxy/welding? And do you have any links to pics? I'm very curious how they got there
There are numerous pics in Leo Santucci's Chevy 6 Performance Handbook. But extensive brazing to the intake ports and very large intake valves are required to reach those flow numbers....I'll see if I can find some pics to share on here...
 
reshaping the ports, we were able to achieve a best of 349 CFM on the intake and around 230 CFM on the exhaust.
I'm curious. Was this an NA application and do you know the HP? I'm wondering how the engine treats the Siamese ports from an area stand point
 
I'm curious. Was this an NA application and do you know the HP? I'm wondering how the engine treats the Siamese ports from an area stand point
Yes, it was naturally aspirated and the last time I saw it dynoed in the late 80's it made 612 HP. By that time the engine was no longer in our Chevy II and was put into a Comp Eliminator rear engine dragster owned by Brian Browell until around 1988, when Brian wanted to take over the driving chores. After switching from the inline power, he switched to the Chevy V6 PowerPlant and had Grumpy Jenkins do his engines until his passing some years back. Brian still races in Comp Eliminator and is the owner of Browell Titanium Bellhousings currently....
 
I'm wondering how the engine treats the Siamese ports from an area stand point
The dynamic port flow for the three Siamese intake ports is different.
If you look at the 1 5 3 6 2 4 firing order, the intake timing for cylinders 3 and 4 have a 360 degree interval and there is no overlap between valve openings in the center intake port.
However, cylinders 1 and 2 have a 240 degree and a 480 degree interval as does cylinders 5 and 6.
When you have a drag racing camshaft lobe profile with well over 240 degrees there will be valve overlap during the 240 degree interval in those ports.
Valve timing can be altered slightly between those cam lobes to decrease the overlap period.
CNC-Dude can shed more light on the subject.

Otherwise, you are looking at a large volume intake port that is relying on the port lump to increase air velocity and tapered rectangular intake manifold runners for velocity and ram.
 
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Here are a couple of pics that Wallen asked for. First, not trying to hijack the thread, but to reinforce what Paul was describing in an outside the box manner of thinking to Wallen and to show with creative thinking what can be accomplished. The top Pic shows the stock intake port with the obnoxious bolt bosses impeding air flow. The middle Pic shows after the bosses removed and the port floor filled by furnace brazing to create a short side radius, or lump as Paul mentioned. The last Pic is the 21st century solution which is a bolt-in lump that is simple to install by most any DIY-er with simple basic tools and at a much cheaper cost. However, they only mimic the street version brazed lump head that the late Kay Sissell offered, but still produces between 260-270 CFM, compared to the factory 160-ish port....
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Here's what the latest technology is in Super Stock cylinder head porting. It retains the factory port volume per the NHRA rules, but flow is increased tremendously over the OEM port location and shape. You could do the same to the Ford 6 ports...
Screenshot_20251130_202440_Samsung Internet.jpg
 
Here's what the latest technology is in Super Stock cylinder head porting. It retains the factory port volume per the NHRA rules, but flow is increased tremendously over the OEM port location and shape. You could do the same to the Ford 6 ports...
View attachment 28229
I have, sorta. I've raised the center of the entry CSA .4". So far the best I can do with out finding water. Note the bottom of the port will be raised by offsetting the intake runner~.3". This got me to 250 CFM. In the hands of a pro I believe this technique would get you close to 260. And yes I have to make an intake manifold.

Link to my progress...

The question I asked myself was how to raise the port without epoxy. After looking at port section pictures I outlined where there was material/opportunity (black lines). Additional background, with flow ball testing I noted extremely fast flow at the roof and limited flow on the floor. So I had a substantial vertical velocity gradient.
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I then realized that the goal is to raise the flow column/cross sectional area as cleanly as possible. Specifically the center of the CSA. Colored lines above approximate the change in the center of the flow path CSA before/after work.

The picture below illustrates the changes in the center of the CSA at the entrance. Yellow is the original center of CSA, Blue is after widening/squaring up the port entry and green is after raising both the roof and the floor. Note the floor is raised using the intake manifold flange and not epoxy (currently). The net effect was to raise the center of the port flow area almost .5"

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The next picture is the outline of my work.

View attachment 27945
Comments on the picture above,
- The second realization was that I needed a larger entry CSA. if I wasn't trying to push my peak HP to higher RPM I may not have widen the port as much as I did. I likely would have just squared it up.
-And the second point is that the horizontal line just above the floor is the approximate amount that I raised the floor.
- The port shape transitions from the outline at the entry to a more standard shape before the short turn (leaned in at the top).
- I ended up shaping the bottom to match the top. Limited impact to flow but notable impact to stability.

End results:
- An improved vertical velocity gradient, flows at the top slowed down and flows on the floor sped up.
- ~20 CFM improvement
- Rock solid stability (when implemented correctly)

I think I've said this before but I need to emphasize that doing this without a flow bench won't work (in my opinion)

I know, you asked "what time is it" and I told you how to build a clock........
 

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