redblockpowered
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- Joined
- May 5, 2015
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- Swampscott, MA
What if... intake runner flaps.
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Like a 4AGE intake? I forget how they implemented the variable intake on that one.What if... intake runner flaps.
I was picturing like an N52 BMW but that too.
Reminds me of the B20 dual butterfly manifold.![]()
Basically - different runner lengths instead of runner areas. I think the 4AGE setup like covers half the runner or something.
Interesting because when I was putting my top end together with Erland Cox his critique of the Nathan manifold was the runners being too short. I believe I have measurements and volume calcs in my stale build thread. I did pull in a ported KLR intake from him but haven’t used it yet. I think Tate is working on doing that swap and pretty interested to see the comparison data.I'm not unhappy with the port DIAMETERS on a B230F but I wish the runners on the intake were about 2" shorter. This would be if I were building a performance engine.
Give me all the data.Interesting because when I was putting my top end together with Erland Cox his critique of the Nathan manifold was the runners being too short. I believe I have measurements and volume calcs in my stale build thread. I did pull in a ported KLR intake from him but haven’t used it yet. I think Tate is working on doing that swap and pretty interested to see the comparison data.
I think some of this is from large runner dia combined with short radii in the velocity stack.Interesting because when I was putting my top end together with Erland Cox his critique of the Nathan manifold was the runners being too short. I believe I have measurements and volume calcs in my stale build thread. I did pull in a ported KLR intake from him but haven’t used it yet. I think Tate is working on doing that swap and pretty interested to see the comparison data.
We had the NIW at overall volume of ~5,445cc and the volume of the runners at 138cc per or 552cc total. This is based on a set of external measurements and math so it’s approximate not a big science project. Could pull numbers from the KL piece sometime I suppose.Give me all the data.
I guess I have to clarify that I'm looking at it from a naturally aspirated perspective, that can compromise some below 3500 or so. Other applications may ask for something different.
It’s interesting that there doesn’t seem to be a lot of data available about boosted engines with runner length tuning. And from my experience it tends to come back to compressed density effects on waveform velocity, etc.
While the speed of sound isn’t affected by air pressure, the theories that have been discussed contribute waveform velocity changes under pressure to the changes in fuel density within the air charge. Having more so to do with what else is in the air when it’s compressed.Speed of sound is not affected by air pressure.
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Speed of sound - Wikipedia
en.wikipedia.org
However, it seems as if turbo intake runners are often shorter than pulse tuned NA runners/intakes.
So good question, does a turbo engine require different intake lengths than a NA engine?
If so, what is the mechanism behind this?
Speed of sound increases with temperature.
According to the formulas, the speed of sound in an ideal gas is proportional to the root of absolute temperature.
However I do not think that with a good turbo/IC setup the intake temperature increase would be that significant as to affect the tuned intake length.
Any opinions?
Edit - A temperature increase (higher speed of sound) would actually require an even longer runner instead of a shorter one.
Density and moisture content definitely have an impact on wave travel speed in air. Higher density and higher moisture equals faster wave speed.While the speed of sound isn’t affected by air pressure, the theories that have been discussed contribute waveform velocity changes under pressure to the changes in fuel density within the air charge. Having more so to do with what else is in the air when it’s compressed.
Density and moisture content definitely have an impact on wave travel speed in air. Higher density and higher moisture equals faster wave speed.
At around 10k ft elevation the speed of sound is roughly 60-70% compared to sea level.
The more molecules the wave can travel through, the faster it will be.
And it’s not just one, two or three variables that we have here. It’s the combinations that bring us to the intriguing phenomenon that make up the discussion.It would be good to differentiate in the cause of the density change.
If the composition changes (injecting fuel) this is the case, yes the speed of sound is affected. However in the case of a density change due to a pressure difference, speed of sound is not affected.
"In the Earth's atmosphere, the chief factor affecting the speed of sound is the temperature. For a given ideal gas with constant heat capacity and composition, the speed of sound is dependent solely upon temperature; see § Details below. In such an ideal case, the effects of decreased density and decreased pressure of altitude cancel each other out, save for the residual effect of temperature."