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600whp on FP red?

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Old Jul 25, 2016 | 10:31 AM
  #16  
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Originally Posted by Erik@MIL.SPEC
Well, technically the FP manifold has runners that are 20% bigger

And you can gain a little bit of area by gasket matching both the exhaust mani exit and the turbine housing entrance. How much extra area, you'd have to get someone who knows how to measure that in regards to the original opening.

And of course, that doesn't solve the 10.5cm problem anyways.




You edited your original comment, which said: "...you will see a bunch of graphs but most cars dont back it up at the track to be honest."

So, which cars are you talking about? Most of these 600whp cars will trap 130+ in the 1/4 mile. Abacus' car is an exception because of the 4.11 FD. And I feel like we've already had this conversation with you regarding the 4.11 FD in a different thread lol
The 10.5cm is the area of the nozzles in the turbine housing (turbine housing inlet), which is also the ares of the outlets on the mani. So, no matter how much porting you do, the biggest it's going to be is 10.5cm^2 because the gasket is likely what is truly 10.5, while the casting ends up undersized.
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Old Jul 25, 2016 | 10:53 AM
  #17  
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Originally Posted by letsgetthisdone
The 10.5cm is the area of the nozzles in the turbine housing (turbine housing inlet), which is also the ares of the outlets on the mani. So, no matter how much porting you do, the biggest it's going to be is 10.5cm^2 because the gasket is likely what is truly 10.5, while the casting ends up undersized.
Oh, really? I did not know that. I thought it had to do with internal turbine housing volume or something.

I found this here: https://www.evolutionm.net/forums/ev...ml#post2769621

"The formula for area is pi * d^2 / 4.

10.5 cm^2 ==> 3.656366396 cm diameter
9.8 cm^2 ==> 3.532385531 cm diameter

So which part of the turbine housing can have such a diameter? Forced Performance has this written on their webpage.

Quote:
What's the difference between 6cm2, 7cm2, and 8cm2 turbine housings?

Contrary to what your friend told you, a 7cm2 turbine housing does not have an inlet that is 7cm across. The 6cm2, 7cm2, and 8cm2 designations given to Mitsubishi turbine housings refer to the area of the cross section of the housing, known as the nozzle area."



So, how do I get someone to measure my gasket then. Also, if true about non-ported units, that means most people running one don't have a 10.5cm housing lol

Also, I checked my MHI housing last night, and it's A3N material...which is a slightly better Herculite formulation from Hitachi. I think my old housing was F5N.

Last edited by Erik@MIL.SPEC; Jul 25, 2016 at 11:01 AM.
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Old Jul 25, 2016 | 11:14 AM
  #18  
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Originally Posted by Erik@MIL.SPEC
Oh, really? I did not know that. I thought it had to do with internal turbine housing volume or something.

I found this here: https://www.evolutionm.net/forums/ev...ml#post2769621

"The formula for area is pi * d^2 / 4.

10.5 cm^2 ==> 3.656366396 cm diameter
9.8 cm^2 ==> 3.532385531 cm diameter

So which part of the turbine housing can have such a diameter? Forced Performance has this written on their webpage.

Quote:
What's the difference between 6cm2, 7cm2, and 8cm2 turbine housings?

Contrary to what your friend told you, a 7cm2 turbine housing does not have an inlet that is 7cm across. The 6cm2, 7cm2, and 8cm2 designations given to Mitsubishi turbine housings refer to the area of the cross section of the housing, known as the nozzle area."



So, how do I get someone to measure my gasket then. Also, if true about non-ported units, that means most people running one don't have a 10.5cm housing lol

Also, I checked my MHI housing last night, and it's A3N material...which is a slightly better Herculite formulation from Hitachi. I think my old housing was F5N.
The 10.5cm^2 is not the diameter of anything, its the "cross sectional area" of the inlets. Since they are not a circle, they don't have a diameter. You really wouldn't be able to measure it by hand since the corners are round. You would need to use a scanner and scan the housing into a modeling software and measure them that way.


If the number was housing volume, it would be a cubed (^3) number, not a squared (^2) number.
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Old Jul 25, 2016 | 11:28 AM
  #19  
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Originally Posted by letsgetthisdone
The 10.5cm^2 is not the diameter of anything, its the "cross sectional area" of the inlets. Since they are not a circle, they don't have a diameter. You really wouldn't be able to measure it by hand since the corners are round. You would need to use a scanner and scan the housing into a modeling software and measure them that way.


If the number was housing volume, it would be a cubed (^3) number, not a squared (^2) number.
Right, sorry. Should have been more clear when I pulled those quotes.

Question is, where does Mitsubishi measure the cross sectional area? Not the actual openings, but probably further in at the scrolls, correct?
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Old Jul 25, 2016 | 11:29 AM
  #20  
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I'm fairly certain its the opening.
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Old Jul 25, 2016 | 11:34 AM
  #21  
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Originally Posted by letsgetthisdone
I'm fairly certain its the opening.
Found this (everything you read on the Internet is true):

The cm^2 that you see on mitsubishi turbines is actually the smallest cross sectional area at the throat of the turbine, right before it opens up and hits the wheel. This tells you a bit about what the velocity will be going into the turbine.

I'm just curious and looking for info at this point.

THat quote came from the 7th post in this thread:

http://www.galantvr4.org/ubbthreads/...page=8&fpart=1

This was also interesting. Porting doesn't change area, but it changes A/R.

"Also, when you port a turbine housing, you are basically changing the A/R ratio by increasing the area. The reason you get better spoolup from porting is that the higher A/R performs better at higher flow and boost pressures. Up to the stock boost level, the turbine will spin up slower, but above that, the lower restriction wins out over the higher velocity because it gets too turbulent (it works exactly like head porting - there's an optimum "mach number" that results in the most efficient flow)."
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Old Jul 25, 2016 | 12:01 PM
  #22  
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Yeah, I'm not sure, I've found conflicting info on where it's measured. Although, the housing gets TINY down by the turbine, so Idk if it's 10.5 down there. It certainly doesn't look like it.
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Old Jul 25, 2016 | 03:05 PM
  #23  
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you are not really gonna find a good explanation of how a/r is calculated. you will find plenty of conflicting info. I started this thread when I was trying to determine what size a/r the new housing I had actually was. I think I have a pretty good grip on what a/r is. its bascally the area above the wheel. called volute. also called snail. also called nozzle area. all referring to same thing. bigger a/r has more area. which both cools and slows the gas.
http://www.dsmtuners.com/threads/6cm...post-153565537
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Old Jul 27, 2016 | 05:42 AM
  #24  
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Way to ruin this mans thread guys LOL
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Old Jul 27, 2016 | 11:13 AM
  #25  
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Originally Posted by Fast_Freddie
Way to ruin this mans thread guys LOL
I feel like we expanded on the discussion with lots of good information
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Old Jul 28, 2016 | 07:01 PM
  #26  
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So, how long until the old MHI housings crack. I am thinking this with a Magnus intake, and an optimized intake (cold air) and with the car I am thinking of getting I can be close to 600whp w/o over-spinning the turbo on E85. That being said, 575 is just as good if it is FUN FACTOR/TORQUE.
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Old Jul 28, 2016 | 07:22 PM
  #27  
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First thing you want to do is look and see if the housing says F5N or A3N. Those are two different formulations of Hercunite from Hitachi. The A3N can resist temperatures of up to 950* C, while the F5N has an upper limit of 900* C.

http://www.hitachi-metals.co.jp/e/pr...eg/p06_01.html

I checked, and luckily mine is A3N. I also got mine cryotreated and ceramic coated inside and out. Not sure if the cryotreating will help, but it was cheap. THe ceramic coating should definitely help keep heat out of the housing.
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