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Twin scroll T3 manifold

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Old Apr 23, 2007 | 08:23 PM
  #106  
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Mass or volume?

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Old Apr 23, 2007 | 08:25 PM
  #107  
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Neither, it would be area.

If it isn't (and I don't know that to be the case), that would appear to be some 10-15% of the total area. That would effectively make a .70 fall somewhere between a .63-.61 A/R in conventional terms.
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Old Apr 23, 2007 | 08:33 PM
  #108  
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Ted how would it be area? Isn't area just to do with surface where as volume has to do with the space it actually occupies?

Looking directly at the divided t3 flange the "area" it takes up is quite minimal compaired to the amount of volume it takes up, no?

->trying to learn, I have found you are wise

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Old Apr 23, 2007 | 08:46 PM
  #109  
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A/R is a measure of the cross sectional area divided by the radius at any given point. This does not consider volume, only the cross section.

If the volume were likewise 10-15% smaller for a given A/R as compared to a conventional type housing, this could conceivably impact residual pressure at higher engine speeds, but I certainly can't speculate further.
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Old Apr 23, 2007 | 08:56 PM
  #110  
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Originally Posted by Ted B
A/R is a measure of the cross sectional area divided by the radius at any given point. This does not consider volume, only the cross section.

If the volume were likewise 10-15% smaller for a given A/R as compared to a conventional type housing, this could conceivably impact residual pressure at higher engine speeds, but I certainly can't speculate further.
In every description I have ever read about area it is described as the open inner area of the volute, and to me indicates that it is the open space not the space taken by any portion of the turbine housing. If one were to assume any thing, wouldn't it be that the divider is accounted for? (I do not know for sure either, just trying to help work this out)
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Old Apr 23, 2007 | 09:12 PM
  #111  
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Yes, it would be essentially the I.D. of the volute, not the O.D. That does imply the divider is accounted in the calculation, and is what I would assume by default unless informed otherwise. After all, it wouldn't seem to make much sense to pretend it wasn't there when the engineers made those calcs.
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Old Apr 23, 2007 | 10:58 PM
  #112  
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Rest assured that the "A" (in A/R) of twin scroll housings represents the area of the actual flow paths of the volute. The area of the divider wall is not factored in.

Just to beat this to its engineering geekery extreme, "A" is the radial cross-sectional area of the flow path of the volute at the first section which is open to the wheel's inducer (where the tongue of the housing is). The "R" is the radius of the centroid of that cross-sectional area.

As you progress along the volute, the A decreases (until zero, duh) much faster than the R does, meaning A/R is not constant for the entire volute. So, the A/R of a housing is defined at that section located right at the tongue.
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Old Apr 24, 2007 | 12:07 AM
  #113  
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Originally Posted by JKav
Rest assured that the "A" (in A/R) of twin scroll housings represents the area of the actual flow paths of the volute. The area of the divider wall is not factored in.

Just to beat this to its engineering geekery extreme, "A" is the radial cross-sectional area of the flow path of the volute at the first section which is open to the wheel's inducer (where the tongue of the housing is). The "R" is the radius of the centroid of that cross-sectional area.

As you progress along the volute, the A decreases (until zero, duh) much faster than the R does, meaning A/R is not constant for the entire volute. So, the A/R of a housing is defined at that section located right at the tongue.
So in short, a twin scroll .78 A/R housing should have the same potential for flow as a .78 A/R undivided housing (not accounting for the advanced distribution of properly constructed divided manifolds with divided turbine housing)?
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Old Apr 24, 2007 | 06:07 AM
  #114  
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Originally Posted by JKav
As you progress along the volute, the A decreases (until zero, duh) much faster than the R does, meaning A/R is not constant for the entire volute. So, the A/R of a housing is defined at that section located right at the tongue.
FWIW, according to Corky Bell, the A/R is constant up to the exducer. If the measurements are taken at seveal points along the flowpath, one gets:

A1/R1 = A2/R2 = A3/R3, and so forth.
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Old Apr 24, 2007 | 06:36 AM
  #115  
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I guess my post got missed in teh mix, lol
How are you guys making out with your manifold coating from jethot. Durability any good.
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Old Apr 24, 2007 | 06:50 AM
  #116  
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FYI: This is a discussion on divided manifolds and turbine housings, not coatings. There are other discussions for that. Use the 'search' feature.
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Old Apr 24, 2007 | 07:31 AM
  #117  
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Originally Posted by Ted B
FWIW, according to Corky Bell, the A/R is constant up to the exducer. If the measurements are taken at seveal points along the flowpath, one gets:

A1/R1 = A2/R2 = A3/R3, and so forth.
Think about it. In the limit, the area approaches zero whereas the radius approaches that of the wheel (+ clearance to the housing).

Even just halfway around the volute, the A is halved, but the R is not even close to halved (if it was, you'd be in the wheel).

This is why A/R is defined at one specific section.
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Old Apr 24, 2007 | 07:37 AM
  #118  
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Originally Posted by StyleFront
So in short, a twin scroll .78 A/R housing should have the same potential for flow as a .78 A/R undivided housing (not accounting for the advanced distribution of properly constructed divided manifolds with divided turbine housing)?
Twin scrolls often flow a hair less at equivalent a/r as boundary layer effects come into play.

Efficiency-wise, twin scrolls take a small hit due to increased 'wetted' surface area imposed by the divider wall. However, this is way more than offset by the vastly superior pulse conversion you get.

Edit: I should probably clarify that last bit. Twin scroll turbines, as mapped on a gas stand (steady state conditions) will exhibit a slight drop in efficiency compared to an otherwise equivalent non-divided housing. On-engine, however, is much different. The flow conditions are highly unsteady. The ability of a twin scroll to utilize the pulsing, unsteady flow of the exhaust exiting the engine gives it a huge bump in "apparent" efficiency, and ultimately spools up the turbine that much sooner.

Twinscrolls also isolate the cylinders' blowdown events much better than a non-divided housing, preventing the exhausting cylinder's very high PEAK exhaust manifold pressures from finding their way into the other cylinder on its overlap period.

Last edited by JKav; Apr 24, 2007 at 08:26 AM.
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Old Apr 24, 2007 | 07:55 AM
  #119  
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Originally Posted by Frenchy4g63
The HTA turbo's are a line of custom compressor wheels designed by FP. Dave Buschur has one, the only one as far as I know, and it makes a little more power than a standard 35r. But, it makes a lot more midrange power, spools faster, just better in every way.

So I'm thinking about doing a twin scroll T4 flanged manifold, with a .85 a/r T4 twin scroll turbine housing on the HTA 35r. Which is why Ted mentioned the T4 housings.

Basically a twin scroll T4 35r, with better midrange and quicker spool, due to the HTA wheel and the twin scroll design.

The .78 a/r T3 housing your mentioning uses a divided housing. Generally when you go to a twin scroll setup, you need to use larger than normal turbine housings. Personally I believe that housing is too small for a 3082/3065. I still think it would be become a restriction on a 3076 if you were trying to max it out. Although according to TedB, it works very, very well.

The 3065, 3082, and HKS 3037, are all the same turbo, just different names.
the 3065/3082 have a 82mm compressor wheel. the 3037/3076 have a 76.2mm compressor wheel. this statement is false as far as i know.

Last edited by deadbeatrec; Apr 24, 2007 at 08:01 AM.
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Old Apr 24, 2007 | 09:27 AM
  #120  
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Originally Posted by deadbeatrec
the 3065/3082 have a 82mm compressor wheel. the 3037/3076 have a 76.2mm compressor wheel. this statement is false as far as i know.
+1
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