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350whp on 92 octane - How do I get there?

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Old 12-19-2009 | 09:19 AM
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Well the typical rule is to keep exhaust gas velocity below 250ft/sec.
Using:

Airflow / Area = 250

I get ~2.7inch diameter pipe would be the minimum for post turbine... Pre-turbine, we can usually get away with a bit smaller, to help drive the turbo.


-Rogue
Old 12-19-2009 | 09:46 AM
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And if anyone felt so inclined, these guys could tell you, with extreme precision, what size and your exhaust should be:

Burns Stainless
Old 12-19-2009 | 08:58 PM
  #108  
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How is exhaust seen as a fluid? I'd never heard that.
Old 12-19-2009 | 09:24 PM
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Originally Posted by Rogue_Ant
Well the typical rule is to keep exhaust gas velocity below 250ft/sec.
Using:

Airflow / Area = 250

I get ~2.7inch diameter pipe would be the minimum for post turbine... Pre-turbine, we can usually get away with a bit smaller, to help drive the turbo.


-Rogue
Would the crossover ID be any different on our engines between a GT30 and GT35 turbo's (I know the hot side size is what would matter)? Generally speaking....

I would think, with the crossover, that erroring on the big side would be better than too small right? A little extra lag is better than loss of boost at the top?
Old 12-19-2009 | 09:32 PM
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Originally Posted by m73m95
Would the crossover ID be any different on our engines between a GT30 and GT35 turbo's (I know the hot side size is what would matter)? Generally speaking....

I would think, with the crossover, that erroring on the big side would be better than too small right? A little extra lag is better than loss of boost at the top?
ID is determined by max airflow... So if both turbos are running the same airflow, then the ID would be the same.
And generally, pre-turbine its better to error on the smaller side then larger.
So with my example earlier, it would be better to run 2.5" rather then 3".


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Old 12-19-2009 | 09:45 PM
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Why would you go smaller?

Didn't this thread say, a few pages ago, that to much back pressure in the crossover was a bad thing?

There's quite a big difference between 2.5 and 3in anyway.... I was thinking on the lines of 2.25 vs 2.5 (or am I WAY over thinking the crossover?)
Old 12-20-2009 | 03:04 AM
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You are over thinking it, lol
Backpressure is mainly determined by the turbine section of the turbo, much less so the crossover pipe-diameter. The turbine inlet is only so big, and really, going any larger on crossover pipe size does not make a whole lot of sense.
Old 12-20-2009 | 03:06 AM
  #113  
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I'm finding that I know just enough about forced induction to be dangerous

NA stuff, I'm the man. Turbo.... Guess I'm still learning.
Old 12-20-2009 | 03:21 AM
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A great book to build turbo knowledge is "Maximum Boost by Corky Bell". It has been the staple for turbocharging for years.

Maximum Boost
Old 12-20-2009 | 04:39 AM
  #115  
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corky bell has a book on any topic you will ever want to know about
Old 12-20-2009 | 09:57 AM
  #116  
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I'm also in the camp that thinks that the turbine is the most important aspect of determining the back pressure at the exhaust valve.
So, what would be the significance of modifying the headers, which I've heard about over time?
Old 12-20-2009 | 11:14 AM
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Originally Posted by gruhsy
Yes and no. I had a friend tell me recently that worked for Honda superbike race team that exhaust is like black magic. I am no expert on the 944 turbo exhaust but from Power Engineering I know that we calculate pipe diameter and tubing size based on temperatures and fluid being moved.

When you look a sport bikes people buy various tuned exhaust system. Eg Muzzy, Yoshomura, Akrapovic, etc. They don't just have a local exhaust shop weld up a pipe system. Exhaust should all be about tuning to me since thats what streetbikes do.

We do know we are limited by the turbo inlet size so anything bigger than that is pointless. Exhaust also bounces as a wave through the system. Changing shapes and diameters changes tuning properties. Eg equal length headers.
I will dig through some of my PE books and see if I can find something that might anwer that question better. Again I'm no expert but I have been thinking about that for a while since I am in the middle of having my 3.0 built.

Jason
This is not the case. Look at the stacks on a Nuclear power plant. They are not cylindrical, they are converging and diverging. This is so they can move more H20 (coolant) so the plant doesn't have to be shut down due to cooling issues.

It's the same principle with exhausts. I'm not saying you want the crossover diameter to be larger than the turbine inlet, but you might gain some exhaust gas velocity through the turbine by keeping the crossover dia slightly larger than the turbine inlet, then just before the turbine inlet, reducing the diameter with a nice reverse cone pipe (instead of one stepped pipe with a sharpe transition).
Old 12-21-2009 | 11:37 AM
  #118  
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Is there a way to create a collector with the exhaust to actually pull out exhaust and thus decrease backpressure?

What about some sort of "velocity stack" approach?
Old 12-21-2009 | 12:00 PM
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Originally Posted by 333pg333
How is exhaust seen as a fluid? I'd never heard that.

http://en.wikipedia.org/wiki/Fluid_dynamics

-Dana
Old 12-21-2009 | 02:07 PM
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Originally Posted by 944CS
This is not the case. Look at the stacks on a Nuclear power plant. They are not cylindrical, they are converging and diverging. This is so they can move more H20 (coolant) so the plant doesn't have to be shut down due to cooling issues.
i believe this is the same idea as tapered intake runners; the stack gets narrower to increase gas velocity to ensure the steam gets out rather than just hanging around and like you said causing cooling issues. then the larger diameter above the "waist" of the stack probably creates a lower pressure area which the gas below will want to flow to.



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