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Old 09-02-2009, 10:27 AM   #1
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Default Turbo Exhaust Theory, The Gospel According to Garrett

Used without permission by Sixshooter:

Turbo Exhaust Theory


I stumbled across this information on a forum.

The following excerpts are from Jay Kavanaugh, a turbosystems engineer at Garrett, responding to a thread on Impreza.net regarding exhaust design and exhaust theory:


Howdy,

This thread was brought to my attention by a friend of mine in hopes of shedding some light on the issue of exhaust size selection for turbocharged vehicles. Most of the facts have been covered already. FWIW I'm an turbocharger development engineer for Garrett Engine Boosting Systems.


N/A cars: As most of you know, the design of turbo exhaust systems runs counter to exhaust design for n/a vehicles. N/A cars utilize exhaust velocity (not backpressure) in the collector to aid in scavenging other cylinders during the blowdown process. It just so happens that to get the appropriate velocity, you have to squeeze down the diameter of the discharge of the collector (aka the exhaust), which also induces backpressure. The backpressure is an undesirable byproduct of the desire to have a certain degree of exhaust velocity. Go too big, and you lose velocity and its associated beneficial scavenging effect. Too small and the backpressure skyrockets, more than offsetting any gain made by scavenging. There is a happy medium here.


For turbo cars, you throw all that out the window. You want the exhaust velocity to be high upstream of the turbine (i.e. in the header). You'll notice that primaries of turbo headers are smaller diameter than those of an n/a car of two-thirds the horsepower. The idea is to get the exhaust velocity up quickly, to get the turbo spooling as early as possible. Here, getting the boost up early is a much more effective way to torque than playing with tuned primary lengths and scavenging. The scavenging effects are small compared to what you'd get if you just got boost sooner instead. You have a turbo; you want boost. Just don't go so small on the header's primary diameter that you choke off the high end.


Downstream of the turbine (aka the turboback exhaust), you want the least backpressure possible. No ifs, ands, or buts. Stick a Hoover on the tailpipe if you can. The general rule of "larger is better" (to the point of diminishing returns) of turboback exhausts is valid. Here, the idea is to minimize the pressure downstream of the turbine in order to make the most effective use of the pressure that is being generated upstream of the turbine. Remember, a turbine operates via a pressure ratio. For a given turbine inlet pressure, you will get the highest pressure ratio across the turbine when you have the lowest possible discharge pressure. This means the turbine is able to do the most amount of work possible (i.e. drive the compressor and make boost) with the available inlet pressure.


Again, less pressure downstream of the turbine is goodness. This approach minimizes the time-to-boost (maximizes boost response) and will improve engine VE throughout the rev range.


As for 2.5" vs. 3.0", the "best" turboback exhaust depends on the amount of flow, or horsepower. At 250 hp, 2.5" is fine. Going to 3" at this power level won't get you much, if anything, other than a louder exhaust note. 300 hp and you're definitely suboptimal with 2.5". For 400-450 hp, even 3" is on the small side.

"As for the geometry of the exhaust at the turbine discharge, the most optimal configuration would be a gradual increase in diameter from the turbine's exducer to the desired exhaust diameter-- via a straight conical diffuser of 7-12 included angle (to minimize flow separation and skin friction losses) mounted right at the turbine discharge. Many turbochargers found in diesels have this diffuser section cast right into the turbine housing. A hyperbolic increase in diameter (like a trumpet snorkus) is theoretically ideal but I've never seen one in use (and doubt it would be measurably superior to a straight diffuser). The wastegate flow would be via a completely divorced (separated from the main turbine discharge flow) dumptube. Due the realities of packaging, cost, and emissions compliance this config is rarely possible on street cars. You will, however, see this type of layout on dedicated race vehicles.


A large "bellmouth" config which combines the turbine discharge and wastegate flow (without a divider between the two) is certainly better than the compromised stock routing, but not as effective as the above.


If an integrated exhaust (non-divorced wastegate flow) is required, keep the wastegate flow separate from the main turbine discharge flow for ~12-18" before reintroducing it. This will minimize the impact on turbine efficiency-- the introduction of the wastegate flow disrupts the flow field of the main turbine discharge flow.


Necking the exhaust down to a suboptimal diameter is never a good idea, but if it is necessary, doing it further downstream is better than doing it close to the turbine discharge since it will minimize the exhaust's contribution to backpressure. Better yet: don't neck down the exhaust at all.


Also, the temperature of the exhaust coming out of a cat is higher than the inlet temperature, due to the exothermic oxidation of unburned hydrocarbons in the cat. So the total heat loss (and density increase) of the gases as it travels down the exhaust is not as prominent as it seems.
Another thing to keep in mind is that cylinder scavenging takes place where the flows from separate cylinders merge (i.e. in the collector). There is no such thing as cylinder scavenging downstream of the turbine, and hence, no reason to desire high exhaust velocity here. You will only introduce unwanted backpressure.


Other things you can do (in addition to choosing an appropriate diameter) to minimize exhaust backpressure in a turboback exhaust are: avoid crush-bent tubes (use mandrel bends); avoid tight-radius turns (keep it as straight as possible); avoid step changes in diameter; avoid "cheated" radii (cuts that are non-perpendicular); use a high flow cat; use a straight-thru perforated core muffler... etc.


"Comparing the two bellmouth designs, I've never seen either one so I can only speculate. But based on your description, and assuming neither of them have a divider wall/tongue between the turbine discharge and wg dump, I'd venture that you'd be hard pressed to measure a difference between the two. The more gradual taper intuitively appears more desirable, but it's likely that it's beyond the point of diminishing returns. Either one sounds like it will improve the wastegate's discharge coefficient over the stock config, which will constitute the single biggest difference. This will allow more control over boost creep. Neither is as optimal as the divorced wastegate flow arrangement, however.


There's more to it, though-- if a larger bellmouth is excessively large right at the turbine discharge (a large step diameter increase), there will be an unrecoverable dump loss that will contribute to backpressure. This is why a gradual increase in diameter, like the conical diffuser mentioned earlier, is desirable at the turbine discharge.


As for primary lengths on turbo headers, it is advantageous to use equal-length primaries to time the arrival of the pulses at the turbine equally and to keep cylinder reversion balanced across all cylinders. This will improve boost response and the engine's VE. Equal-length is often difficult to achieve due to tight packaging, fabrication difficulty, and the desire to have runners of the shortest possible length.


"Here's a worked example (simplified) of how larger exhausts help turbo cars:


Say you have a turbo operating at a turbine pressure ratio (aka expansion ratio) of 1.8:1. You have a small turboback exhaust that contributes, say, 10 psig backpressure at the turbine discharge at redline. The total backpressure seen by the engine (upstream of the turbine) in this case is:


(14.5 +10)*1.8 = 44.1 psia = 29.6 psig total backpressure


So here, the turbine contributed 19.6 psig of backpressure to the total.


Now you slap on a proper low-backpressure, big turboback exhaust. Same turbo, same boost, etc. You measure 3 psig backpressure at the turbine discharge. In this case the engine sees just 17 psig total backpressure! And the turbine's contribution to the total backpressure is reduced to 14 psig (note: this is 5.6 psig lower than its contribution in the "small turboback" case).


So in the end, the engine saw a reduction in backpressure of 12.6 psig when you swapped turbobacks in this example. This reduction in backpressure is where all the engine's VE gains come from.


This is why larger exhausts make such big gains on nearly all stock turbo cars-- the turbine compounds the downstream backpressure via its expansion ratio. This is also why bigger turbos make more power at a given boost level-- they improve engine VE by operating at lower turbine expansion ratios for a given boost level.


As you can see, the backpressure penalty of running a too-small exhaust (like 2.5" for 350 hp) will vary depending on the match. At a given power level, a smaller turbo will generally be operating at a higher turbine pressure ratio and so will actually make the engine more sensitive to the backpressure downstream of the turbine than a larger turbine/turbo would.

[/munchies for your mind]
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Old 09-02-2009, 10:35 AM   #2
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Very good read. Thanks for the info!
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Old 09-02-2009, 10:40 AM   #3
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Jay is also a member here....you might remember his lemons winning miata on the portal page....
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Old 09-02-2009, 11:00 AM   #4
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anyone else find it odd that all the turbo know-it-all types are into miatas? corky, jay, ...
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Old 09-02-2009, 11:08 AM   #5
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I don't know anybody's real names but I did read the Lemons threads.
His name does sound familiar now that you mention it, But I would have never put the two together.

We could certainly use a few more real expert opinions in some of our discussions on theory. And on the EPIC Stud thread...
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Old 09-02-2009, 11:18 AM   #6
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so...what about the huge bell-mouth on my tial turbine housing? Should I be worried about "unrecoverable dump loss"?
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Old 09-02-2009, 11:57 AM   #7
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Hustler, looking at your turbo you are closer to the hyperbolic shape that is stated as ideal than to the step outlet that is listed as having unrecoverable losses.

A step outlet would be more like a straight turbine outlet of 2" being plumbed into a pipe of 3". You will introduce turbulence due to undefined boundary edges. With your bell shaped outlet you have well defined, gradual, laminar flow at the boundary.

For the step, think of a circular vortex that would create little sideways tornados, with all their pressure fluctuations causing flow instability (turbulent flow) instead of the laminar flow you want for maximum gas throughput.
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Old 09-02-2009, 12:20 PM   #8
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Quote:
Originally Posted by hustler View Post
so...what about the huge bell-mouth on my tial turbine housing? Should I be worried about "unrecoverable dump loss"?
your turbine housing is pretty much what jay suggests using.
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Old 09-02-2009, 01:33 PM   #9
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Quote:
Originally Posted by hustler View Post
so...what about the huge bell-mouth on my tial turbine housing? Should I be worried about "unrecoverable dump loss"?
Again you are smoking crack. You worry me. TiAL casts a beautiful cone transition into their turbines.

Did you look at it before you sent it to me?

EDIT: Did you look at your avatar picture? sigh.
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Old 09-02-2009, 03:19 PM   #10
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Quote:
Originally Posted by TurboTim View Post
Again you are smoking crack. You worry me. TiAL casts a beautiful cone transition into their turbines.

Did you look at it before you sent it to me?

EDIT: Did you look at your avatar picture? sigh.
I've never actually seen it in person. Just because some company sold me this crap for $400 doesn't mean they knew what they were doing. I plan for the worst, for a reason.

FYI...I don't exactly to make it to the track with my car...ever. Its just a reasonable goal.
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Old 09-02-2009, 04:17 PM   #11
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Excellent read, thanks
Hustler no worries for the reasons stated above. You are fine. I am not talking out of my *** here; I developed the diffuser for our FSAE throttle/restrictor assembly back in the day.
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Old 09-02-2009, 09:18 PM   #12
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A. Graham Bell's Forced Induction Performance Tuning.

Everything said by Jay is in there as well as all the maths for it and MUCH more. Maybe I'm a bookworm for this stuff but I have a 2ft shelf of this stuff including aero by Simon MacBeth and Electrics by Jon Lawes (my friend )
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