XKR Super G... Going for Mach 1
#1121
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#1122
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EDIT: In the spreadsheet, I use Garrett's published data for the turbine diameter and A/R. Then I assumed the same value for the turbine housing wall thickness and gap between the turbine blades and the wall. The rest is all based on calculations. You will see when you look at the spreadsheet.
Last edited by ttg35fort; 09-13-2009 at 10:10 AM.
#1124
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http://www.xtrac.com/pdfs/386%20Gran...ox%20Jun07.pdf
Transfer weight from the front of the car and get it over the rear wheels. Not only will it help straight line traction, it also should help handling. With the turbo kits, our cars get a little nose heavy. A transaxle will balance it out a bit.
Dog gears are a little rough on the street, though. One of the British companies makes an H-pattern synchromesh transaxle that will work too.
Then again, you can always get hold of one of those Getrag twin-clutch jobs like they use in the Ferraris.
I know, they are all big, big bucks, but if I ever hit the lotto transaxle here I come.
#1125
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twin 67mm turbos should make a TON of power. well north of 1300. How wide of a slick can that car fit? a 12"x28+" slick would be awesome!
I dd it at 14psi, when out with "friends" on pump I'll go to 17psi....have seen 18psi, but the last plug change showed some speckles....so keeping it below that for safety. If we touched the tune could go higher....
But 14psi is 530rwhp (SP's mustang dyno), so figure 18-20hp per lb of boost, so somewhere right at 590-600rwhp at 17psi (have to dyno it at 17psi on pump one day to see)
basically pump gas is more than enough for 99.99% of the stuff out there......but Vlad's crazy G35 sedan just made 597rwhp at 12psi through a TH400.......I'll need a whole lot more for that lol.
tom
But 14psi is 530rwhp (SP's mustang dyno), so figure 18-20hp per lb of boost, so somewhere right at 590-600rwhp at 17psi (have to dyno it at 17psi on pump one day to see)
basically pump gas is more than enough for 99.99% of the stuff out there......but Vlad's crazy G35 sedan just made 597rwhp at 12psi through a TH400.......I'll need a whole lot more for that lol.
tom
#1126
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Garrett finally got back to me, which changes the entire analysis... I updated the post.
Essentially A is the inlet area, but the formula only works in INCHES, while all of their dimensions are specified in mm.
Using A as the area of the inlet (in inches), I computed the turbine inlet areas by converting to inches, performing the calculations, then converting back to mm (only in America do we have to go through this BS - even the British have dropped the British measurement system, for the most part).
Summary is that the T25 flange will work perfectly fine on the turbos we use, even the GT3582R turbos.
Essentially A is the inlet area, but the formula only works in INCHES, while all of their dimensions are specified in mm.
Using A as the area of the inlet (in inches), I computed the turbine inlet areas by converting to inches, performing the calculations, then converting back to mm (only in America do we have to go through this BS - even the British have dropped the British measurement system, for the most part).
Summary is that the T25 flange will work perfectly fine on the turbos we use, even the GT3582R turbos.
Last edited by ttg35fort; 09-14-2009 at 10:58 AM.
#1127
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Garrett finally got back to me, which changes the entire analysis... I updated the post.
Essentially A is the inlet area, but the formula only works in INCHES, while all of their dimensions are specified in mm.
Using A as the area of the inlet (in inches), I computed the turbine inlet areas by converting to inches, performing the calculations, the converting back to mm (only in America do we have to go through this BS - even the British have dropped the Brittish measurement system, for the most part).
Summary is that the T25 flange will work perfectly fine on the turbos we use, even the GT3582R turbos.
Essentially A is the inlet area, but the formula only works in INCHES, while all of their dimensions are specified in mm.
Using A as the area of the inlet (in inches), I computed the turbine inlet areas by converting to inches, performing the calculations, the converting back to mm (only in America do we have to go through this BS - even the British have dropped the Brittish measurement system, for the most part).
Summary is that the T25 flange will work perfectly fine on the turbos we use, even the GT3582R turbos.
#1129
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I wonder if he even new that A/R was a ratio that would only work in inches??? I doubt most people even think too much about this. I didn't until the question about whether the T25 flange was going to be a bottle neck came up. After all of the analysis, it is pretty clear that it won't be. The analysis would have been much faster and easier if Garrett had been more accurate with the information on their website, though.
In fact, Garrett's technical support didn't even immediately know why the A/R ratio was not working. They sent me an e-mail on Friday saying that they needed time to look into the issue. The e-mail I received today indicated that you must use inches for the ratio to work.
It would be helpful for them to update their website with this, considering all of their published dimensions are in mm. Considering their reputation, you would think they would be a little less sloppy about these things.
In fact, Garrett's technical support didn't even immediately know why the A/R ratio was not working. They sent me an e-mail on Friday saying that they needed time to look into the issue. The e-mail I received today indicated that you must use inches for the ratio to work.
It would be helpful for them to update their website with this, considering all of their published dimensions are in mm. Considering their reputation, you would think they would be a little less sloppy about these things.
Last edited by ttg35fort; 09-14-2009 at 11:41 AM.
#1130
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interesting about the calculations.
i guess we'll just have to wait for more real world data becuase if the T25 housing isnt causing excessive backpressure, no one has really even maxxed out the smallest gt3071 yet (which should be around 900 on a dynojet)
i guess we'll just have to wait for more real world data becuase if the T25 housing isnt causing excessive backpressure, no one has really even maxxed out the smallest gt3071 yet (which should be around 900 on a dynojet)
Last edited by str8dum1; 09-14-2009 at 12:16 PM.
#1132
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Moreover, a good wastegate/dump should help to reduce back pressure. Once the pressure that is needed to spool the turbines for the desired intake manifold pressure (MAP) is reached, the wastegates will open. You will know they are adequate if you don't experience boost creep. If boost creep occurs, then you need a larger wastegate.
To get any realizeable benefit out of the T3 or T4 flange, you will need a header style manifold with large tubes. As we discussed, this may not be a viable option for those of use who intend on road racing our cars. As Mike and Roger at Japtrix will attest, SS header style manifolds start to sag over time when used in road racing. Both of these people steared me toward using cast iron manifolds for road racing.
For street and 1/4 mi. use, the SS header style manifolds are the way to go. Still, you need a good wastegate/dump setup because there is always going to be a bottle neck at the turbine inlet.
Also, as you increase the volume of the manifolds, you decrease turbo response (i.e. increase the response time). pV=nRT. So, p=(nRT/V). Assume that nRT is relatively constant at a given moment in time; as V increases p decreases. So R has to increase, which takes a little more time, in order to get the same pressure (R is number of moles of gas). In other words, you need more exhaust gas to build up in the manifold to reach the same pressure. In actuality, T will be slightly lower in a larger manifod because there is more surface area to thermally conduct heat out of the exhaust gases into the engine compartment. So that adds a little bit of time to the spool up as well.
The additional time can be computed based on the amount of air/fuel mixture being combusted and the rate of thermal exchange between the manifold and the ambient air in the engine comparment. Considering, though, that we usually have a fairly large intake systems with all of the piping and the intercooler, the additional turbo lag caused by a bigger exhaust manifold is farely insignificant in the overall scheme of things, and may not be too noticable, if at all. I only went through the logical steps to help increase understanding of the thermodynamics involved for those that are interested.
Last edited by ttg35fort; 09-14-2009 at 03:34 PM.
#1133
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ok so the inlet is ok, what about the outlet?
ATPs custom t25 housing uses a T3 outlet.
http://www.atpturbo.com/Merchant2/me...egory_Code=GTH
any idea there on measurements of the t25 housing outlet?
ATPs custom t25 housing uses a T3 outlet.
http://www.atpturbo.com/Merchant2/me...egory_Code=GTH
any idea there on measurements of the t25 housing outlet?
Last edited by str8dum1; 09-14-2009 at 03:05 PM.
#1134
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ok so the inlet is ok, what about the outlet?
ATPs custom t25 housing uses a T3 outlet.
http://www.atpturbo.com/Merchant2/me...egory_Code=GTH
any idea there on measurements of the t25 housing outlet?
ATPs custom t25 housing uses a T3 outlet.
http://www.atpturbo.com/Merchant2/me...egory_Code=GTH
any idea there on measurements of the t25 housing outlet?
http://www.turbobygarrett.com/turbob...T3071R_new.pdf
The cross sectional area is 4070 mm^2.
The models with the T25 flange are internally wastegated, so the outlet is a completely different shape. It is a "5 Bolt" outlet:
http://www.turbobygarrett.com/turbob...2_3_20_new.pdf
I just did a very quick estimate of the cross-sectional area, but it looks like it is right about the same size.
Note that GTM has disabled the internal wastegate because it does not work as well as an external wastegate.
If anyone wants to take the time to compute the actual cross-sectional area of the 5 Bolt outlet, please do so. It is a relatively complex shape and will take a bit of time. From my perspective, it is a moot point as my estimate will be pretty close. It may turn out that the 5 Bolt outlet is slightly bigger or slightly smaller, but it won't be by much. It appears that Garrett tried to keep the same cross-sectional area as the 3" outlet.
EDIT: Also note that the cross-sectional area of the wastegate will come into play once the desired MAP is acheived. Any excess pressure beyond that which is needed to get the desired MAP will be relieved through the wastegate, assuming the wastegate/dump is large enough to prevent boost creep. Essentially, once the pressure at the turbine reaches the point to give the desired MAP, the wastegate will open and route any additional exhaust gases to the dump.
In summary, the only way a T3 or T4 flange will make a noticable difference is if the size of the exhaust manifold tubes also are increased. Then the net back pressure will be lower. For a log style manifold, it won't make much of a difference.
With respect to the turbine A/R, a smaller A/R will need a bit more pressure to get the same MAP as a turbine with a larger A/R because of the difference in the direction of the exhaust gas flow. Other than this, the wastegate and dump should act to equalize any differences between the turbine housings. A larger A/R will provide more boost potential. However, if a smaller A/R will get you to the boost you need, it is probably a better choice given that it will be more responsive. The pressure differences at the exhaust valves will not be that different among the different A/R turbine housings unless the bottleneck creasted by the exhaust manifold itself is decreased.
Even more summarized, if you have a log style manifold, go with the lower A/R turbine housings and the T25 flange. If you have header style exhaust manifolds with large tubes, go with a T3 or T4 flange. Then you should get a noticable benefit with a larger A/R in terms of lower back pressure at the exhaust valves, as well as greater total boost potential. The cost of this is more turbo lag.
Last edited by ttg35fort; 09-14-2009 at 04:27 PM.