New BW EFR Turbo Thread
If it were really 1% do you think I'd of said anything? Try 10-20%
When I get back home I'll do a model of both a pie cut and a regular exhaust section with mandrel bends in solidworks and show you the flow data. It'll blow your mind. Also I'm curious to see what the delta in flow and back pressure is on 3" mandrel bent and 3.5" pie cut.
All this being said, yes 3.5" is far better than 3" for pretty much anything turbo related.
When I get back home I'll do a model of both a pie cut and a regular exhaust section with mandrel bends in solidworks and show you the flow data. It'll blow your mind. Also I'm curious to see what the delta in flow and back pressure is on 3" mandrel bent and 3.5" pie cut.
All this being said, yes 3.5" is far better than 3" for pretty much anything turbo related.
Marginally.
Neither of them is truly intended to operate in the 1600-1800F range that EGTs get to. To say one is superior is a stretch; while they both offer significant improvement over 304, neither is really the "ideal" material for this application. None of use really blast along at 1600+ EGTs for periods long enough to cause IGC to be a concern either though so it's kind of a moot point.
The head port should actually be larger then the runner diameter to some degree. It should have some excess volume to allow the initial blow-down to exit the valve quickly and then should taper in to recover the velocity as it progresses into the manifold.
I am of the sentiment that you want minimum cross section that can get the job done and focus on stuffing the biggest bend radius in as possible. Bend Radius/Tube Diameter is very important and has a SIGNIFICANT impact on pipe flow losses. I'd rather have a 10% smaller ID and 1.8:1 R/ID ratio then the larger tube with a 1.25 R/ID ratio. That's why I'm not a big fan of weld-els, the bend radius sucks in them.
Hypertune has addressed these issue though by offering bends with larger CLR.
Great looking welds man.
Not all pie-slices are the same man.
Your CFD (appears to be off somebody else's website though?) also looks odd to me as I've done the CFD work along with the basic fluid mechanics courses and that doesn't match conventional pipe flow characteristics. Although, it's highly dependent on the exact bend and flow conditions along with inlet/outlet constraints. Typical turbulent pipe flow though has the highest velocities on the outside of the bend. Too tight of a bend and you end up with flow separation on the inside of the bend which causes eddies to form and huge flow losses.
Pie-slices done correctly however are within a few percent of flow to a mandrel bend of equivalent bend radius. Knowing the correct angles and sizes to get that similar flow characteritic though does take a little bit of knowledge.
But also keep in mind, that "few percent" is based on a PERFECT mandrel bend with zero ovalization of the tube. I've NEVER bought a "perfect mandrel bend" before so I can't really comment on how they really stack up. I can say for certain though, pie-slices done right do have some advantages over mandrel bends in applications that require complex bends.
Neither of them is truly intended to operate in the 1600-1800F range that EGTs get to. To say one is superior is a stretch; while they both offer significant improvement over 304, neither is really the "ideal" material for this application. None of use really blast along at 1600+ EGTs for periods long enough to cause IGC to be a concern either though so it's kind of a moot point.
ha, my manifold is the same internal dia.. 
I came up with it by trying to have the same runner cross section area as the exhaust port... also T4 inlet is slightly larger than the evo exhaust port so I saw no point in having a runner that is significantly smaller than the exhaust port... transitions are the killer..

I came up with it by trying to have the same runner cross section area as the exhaust port... also T4 inlet is slightly larger than the evo exhaust port so I saw no point in having a runner that is significantly smaller than the exhaust port... transitions are the killer..
I am of the sentiment that you want minimum cross section that can get the job done and focus on stuffing the biggest bend radius in as possible. Bend Radius/Tube Diameter is very important and has a SIGNIFICANT impact on pipe flow losses. I'd rather have a 10% smaller ID and 1.8:1 R/ID ratio then the larger tube with a 1.25 R/ID ratio. That's why I'm not a big fan of weld-els, the bend radius sucks in them.
Hypertune has addressed these issue though by offering bends with larger CLR.
Great looking welds man.
If it were really 1% do you think I'd of said anything? Try 10-20%
As you can see it has extremely high velocity right around the angle of the inside of the bend with there being a lower speed boundary layer on the outside of the bend. Having rough corners introduces significantly more turbulence than you'd think which kills flow. I'm actually not sure how much you gain on going from 3" mandrel vs 3.5" pie cut.
Other than the kink bend which might of been a bit of a pie with some bends, mandrels would be better. This is 2015, you can get bends on the internets cheaply and not have to spend hours measuring cutting grinding welding repeat to do pie cuts.
When I get back home I'll do a model of both a pie cut and a regular exhaust section with mandrel bends in solidworks and show you the flow data. It'll blow your mind. Also I'm curious to see what the delta in flow and back pressure is on 3" mandrel bent and 3.5" pie cut.
All this being said, yes 3.5" is far better than 3" for pretty much anything turbo related.
As you can see it has extremely high velocity right around the angle of the inside of the bend with there being a lower speed boundary layer on the outside of the bend. Having rough corners introduces significantly more turbulence than you'd think which kills flow. I'm actually not sure how much you gain on going from 3" mandrel vs 3.5" pie cut.
Other than the kink bend which might of been a bit of a pie with some bends, mandrels would be better. This is 2015, you can get bends on the internets cheaply and not have to spend hours measuring cutting grinding welding repeat to do pie cuts.
When I get back home I'll do a model of both a pie cut and a regular exhaust section with mandrel bends in solidworks and show you the flow data. It'll blow your mind. Also I'm curious to see what the delta in flow and back pressure is on 3" mandrel bent and 3.5" pie cut.
All this being said, yes 3.5" is far better than 3" for pretty much anything turbo related.
Your CFD (appears to be off somebody else's website though?) also looks odd to me as I've done the CFD work along with the basic fluid mechanics courses and that doesn't match conventional pipe flow characteristics. Although, it's highly dependent on the exact bend and flow conditions along with inlet/outlet constraints. Typical turbulent pipe flow though has the highest velocities on the outside of the bend. Too tight of a bend and you end up with flow separation on the inside of the bend which causes eddies to form and huge flow losses.
Pie-slices done correctly however are within a few percent of flow to a mandrel bend of equivalent bend radius. Knowing the correct angles and sizes to get that similar flow characteritic though does take a little bit of knowledge.
But also keep in mind, that "few percent" is based on a PERFECT mandrel bend with zero ovalization of the tube. I've NEVER bought a "perfect mandrel bend" before so I can't really comment on how they really stack up. I can say for certain though, pie-slices done right do have some advantages over mandrel bends in applications that require complex bends.
Fitting that 3.5" downpipe around everything without lowering the crossbrace is some seriously impressive work. I love my MAP O2 eliminator downpipe, but it requires some gigantic crossbrace spacers to fit, leaving the crossbrace hanging lower than I'd like on a street car.
The pie-cut bends may not be ideal, but the 3.5" exhaust already has 36% more cross-sectional area than a 3.0" exhaust, and I doubt a couple of pie-cut bends would come anywhere negating those flow gains.
The pie-cut bends may not be ideal, but the 3.5" exhaust already has 36% more cross-sectional area than a 3.0" exhaust, and I doubt a couple of pie-cut bends would come anywhere negating those flow gains.
sorry but saying 10-20% better flow from those restrictions? I would say you read too much and lack actual testing. I have swapped exhaust on cars and have seen the difference. going from a 3 inch press bend exhaust to an ultra expensive buschur stainless 3 inch mandrel bend exhaust yielded zero HP on a 400whp car.
At only 400hp the restrictions are not relevant. The more pressure and flow you have the more it matters. Try that with 700 and above and report the results. Even 2.75" with smooth bends would be fine for that power envelope. Do not assume that just because you didn't see much of a difference at around 60% of the peak flow of that pipe that there isn't one at higher flow levels.
At only 400hp the restrictions are not relevant. The more pressure and flow you have the more it matters. Try that with 700 and above and report the results. Even 2.75" with smooth bends would be fine for that power envelope. Do not assume that just because you didn't see much of a difference at around 60% of the peak flow of that pipe that there isn't one at higher flow levels.
Is anyone aware of any particular enhanced requirements for oil lines? Either supply or drain? Someone is telling me that the -8 lines are not sufficient and that I need -10. Seems excessive to me. He is currently having problems with one of his turbos smoking and claims that's what is causing it.
Is anyone aware of any particular enhanced requirements for oil lines? Either supply or drain? Someone is telling me that the -8 lines are not sufficient and that I need -10. Seems excessive to me. He is currently having problems with one of his turbos smoking and claims that's what is causing it.
Is anyone aware of any particular enhanced requirements for oil lines? Either supply or drain? Someone is telling me that the -8 lines are not sufficient and that I need -10. Seems excessive to me. He is currently having problems with one of his turbos smoking and claims that's what is causing it.
It still comes down to the fact that the best exhaust for a turbo car is the biggest/least exhaust. Any kind of restriction after the turbine is going to impede performance. Sure there are compromises, but if you can fit a 3.5" downpipe, you should do it.
I definitely think that if you are running a large enough turbo, a 3.5" dp would for sure improve spool and overall response.










