t-61 vs T60-1
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Ted,
Other peoples ignorance justifies you being a jerk to them? I dont think members should have to tip toe around you because they might make an incorrect statement, cuz if they do youll have a "big ****** problem" with it. You may have a lot of knowledge but you treat people like ****. If you treated people like that at a street races, or a track on a daily basis, youd be getting in fights pretty regularly!
Other peoples ignorance justifies you being a jerk to them? I dont think members should have to tip toe around you because they might make an incorrect statement, cuz if they do youll have a "big ****** problem" with it. You may have a lot of knowledge but you treat people like ****. If you treated people like that at a street races, or a track on a daily basis, youd be getting in fights pretty regularly!
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Originally posted by RETed
I put money that 99% of the folks on here don't know...
1) How a turbo works
2) How a waste works
3) How to read compressor maps
4) What A/R stands for
5) How much air flow does a 13B do
6) Difference between boost and airflow
(And the list goes on...)
If they did, we would have a lot less questions.
Asking for help is a little different than claiming you know something when obviously you don't.
I've got a big ****** problem with that.
-Ted
I put money that 99% of the folks on here don't know...
1) How a turbo works
2) How a waste works
3) How to read compressor maps
4) What A/R stands for
5) How much air flow does a 13B do
6) Difference between boost and airflow
(And the list goes on...)
If they did, we would have a lot less questions.
Asking for help is a little different than claiming you know something when obviously you don't.
I've got a big ****** problem with that.
-Ted
of the things you listed...
1) i know that
2) understand, but have never taken apart an external one to really look at it (i learn visually very well) - i would assume very similar to a BOV if i understand it all correctly.
3) How to read compressor maps - a friend of mine helped me to gain a general understanding, but am still learning and would like to learn how to better...
4) What A/R stands for - heard 2 different explanations and read 2 different things in a few websites.
5) How much air flow does a 13B do - dont know
6) Difference between boost and airflow - dont know what you mean by airflow....i am no engine expert
I have no problem admitting that I dont know everything. When i post a question, i try to address any questions and supply what information i know in the begining so that i can go from there or be corrected where i am wrong. so, all of these things that people dont know.....how about you help us all out and make a few threads about it all and give us some reference sources. there are GOING to be people asking questions b/c the whole world is not on your education level on every subject. THAT is the only ignorance that i see on this matter.
Obviously other people respect your opinions and the information that you do provide....shouldnt you give them the same respect back when you provide that information or correct any faults in their statements? I would think so.
---------------------------------------------------------------
NOW....can ANYONE give me information on a T61 with 1.00 exhaust. has anyone used this setup....know someone who has used this setup.....have dyno charts...ANYTHING??
TIA,
#28
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Originally posted by boostmotorsport
Other peoples ignorance justifies you being a jerk to them? I dont think members should have to tip toe around you because they might make an incorrect statement, cuz if they do youll have a "big ****** problem" with it. You may have a lot of knowledge but you treat people like ****. If you treated people like that at a street races, or a track on a daily basis, youd be getting in fights pretty regularly!
Other peoples ignorance justifies you being a jerk to them? I dont think members should have to tip toe around you because they might make an incorrect statement, cuz if they do youll have a "big ****** problem" with it. You may have a lot of knowledge but you treat people like ****. If you treated people like that at a street races, or a track on a daily basis, youd be getting in fights pretty regularly!
-Ted
#29
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Originally posted by suganuma
Obviously other people respect your opinions and the information that you do provide....shouldnt you give them the same respect back when you provide that information or correct any faults in their statements? I would think so.
Obviously other people respect your opinions and the information that you do provide....shouldnt you give them the same respect back when you provide that information or correct any faults in their statements? I would think so.
Since my comments have hit some kinda thorn for some people, maybe I should qualify my statements.  There are ways to get efficiency up on turbo power out.  I'd like to see a 60-1 put out 400RWHP (not 399.999) at 15psi (not 14.999) on a DynoJet (or equivalent) using a A2A FMIC with no other cooling enhancements.  A2W IC's (and any number of ingenious methods to cool the intake charge down) can easily cool to below ambient temps - hell, you can get it down to freezing if you want.  There's a lot of talk of I've-seen-blah-blah-blah - maybe we can get dyno sheets posted here for proof?
-Ted
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Originally posted by RETed
I put money that 99% of the folks on here don't know...
1) How a turbo works
2) How a waste works
3) How to read compressor maps
4) What A/R stands for
5) How much air flow does a 13B do
6) Difference between boost and airflow
(And the list goes on...)
If they did, we would have a lot less questions.
Asking for help is a little different than claiming you know something when obviously you don't.
I've got a big ****** problem with that.
-Ted
I put money that 99% of the folks on here don't know...
1) How a turbo works
2) How a waste works
3) How to read compressor maps
4) What A/R stands for
5) How much air flow does a 13B do
6) Difference between boost and airflow
(And the list goes on...)
If they did, we would have a lot less questions.
Asking for help is a little different than claiming you know something when obviously you don't.
I've got a big ****** problem with that.
-Ted
I 've been trying to find this out for a while
Gene
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Hes right when he said that most people on this forum dont know..... All I am saying is even if thats true it doesnt necessitate being a jerk to them for it. I wonder if he acts that way when he hears a incorrect/untrue statement about subjects other than cars. I am just tired of hearing him bash people just because he disagrees. hes just a lil arrogant in my opinion, knowledgable but arrogant.
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Originally posted by RETed
I hope you're not implying that you can compare rotary turbo power versus piston turbo power.  Typically, power figures are lower on a rotary by almost 20% compares to an identical turbo on a piston engine.
-Ted
I hope you're not implying that you can compare rotary turbo power versus piston turbo power.  Typically, power figures are lower on a rotary by almost 20% compares to an identical turbo on a piston engine.
-Ted
Why does a rotary have a 20% handycap for a piston engine? Are you comparing similarly sized engines. I'm not saying it is or isnt I'm just asking why a rotart would have a 20% decrease in hp over a 2.6L piston engine with the same turbo and the same boost with all other things being equal like air temps ect...
Is it because a piston engine can breath more air? Well, I guess if they are the same size they should take in about the same amount of air?
Please explain Ted, you've got me thinking and now I cant work!!!!! Damn, you lol
STEPHEN
Last edited by SPOautos; 06-11-02 at 11:47 AM.
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Originally posted by SPOautos
Why does a rotary have a 20% handycap for a piston engine? Are you comparing similarly sized engines. I'm not saying it is or isnt I'm just asking why a rotart would have a 20% decrease in hp over a 2.6L piston engine with the same turbo and the same boost with all other things being equal like air temps ect...
Is it because a piston engine can breath more air? Well, I guess if they are the same size they should take in about the same amount of air?
Please explain Ted, you've got me thinking and now I cant work!!!!! Damn, you lol
STEPHEN
Why does a rotary have a 20% handycap for a piston engine? Are you comparing similarly sized engines. I'm not saying it is or isnt I'm just asking why a rotart would have a 20% decrease in hp over a 2.6L piston engine with the same turbo and the same boost with all other things being equal like air temps ect...
Is it because a piston engine can breath more air? Well, I guess if they are the same size they should take in about the same amount of air?
Please explain Ted, you've got me thinking and now I cant work!!!!! Damn, you lol
STEPHEN
The basic formula to calculate engine flow for a turbo application involves a number of factors:
engine displacement, cubic inches (D)
volumetric efficiency (VE)
max RPM (RPM)
displacement/rev (D_R)
conversion factor (1728)
thus:
D x VE x RPM x D_R / 1728
For a nonported rotary:
80 x .70 x 8500 x 1/1728 = 296 CFM (assuming my VE is correct!)
For a 2.6 liter boinger:
160 x .85 x 8500 (yeah right) x 2/1728 = 334
334= 12.5 % greater than the rotary's 296, but there is at least one other factor to consider (below).
Couple of remarks-
A piston engine only displaces half of its volume per revolution, while the rotary displaces all of it's volume per rev. That will change the 13B displcement from 1.3L to 2.6. I think rotary engines have a lower VE than piston engines (and used .7 versus .85), which might explain Ted's 20% estimate.
If this is true, however, then the 20% will diminish if the rotary is ported.
The other factor to consider is exhaust gas temperature which I think is much higher on a rotary compared to a piston engine.
Gene
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A few things.
One, I personally don't mind an attitude if I am getting something (good reliable information) out of the conversation.
Two, you still need to convert cfm to lb/min if you are going to use the info to read and plot compressor maps. They all show in lbs/min nowadays. But I think you calcualtions are right. I have in my mind something like 300cfm for a stock port 13b.
Anybody know how to convert cfm to lb/min?
One, I personally don't mind an attitude if I am getting something (good reliable information) out of the conversation.
Two, you still need to convert cfm to lb/min if you are going to use the info to read and plot compressor maps. They all show in lbs/min nowadays. But I think you calcualtions are right. I have in my mind something like 300cfm for a stock port 13b.
Anybody know how to convert cfm to lb/min?
Last edited by machinehead; 06-11-02 at 08:24 PM.
#35
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Originally posted by SPOautos
Why does a rotary have a 20% handycap for a piston engine? Are you comparing similarly sized engines. I'm not saying it is or isnt I'm just asking why a rotart would have a 20% decrease in hp over a 2.6L piston engine with the same turbo and the same boost with all other things being equal like air temps ect...
Is it because a piston engine can breath more air? Well, I guess if they are the same size they should take in about the same amount of air?
Why does a rotary have a 20% handycap for a piston engine? Are you comparing similarly sized engines. I'm not saying it is or isnt I'm just asking why a rotart would have a 20% decrease in hp over a 2.6L piston engine with the same turbo and the same boost with all other things being equal like air temps ect...
Is it because a piston engine can breath more air? Well, I guess if they are the same size they should take in about the same amount of air?
*Decreased efficiency of the rotor combustion "chamber" versus the round combustion chamber of a piston engine - i.e. more complete burn in a piston engine.
*Relatively early opening of the exhaust port versus the piston exhaust valve timing - if combustion is kept longer inside the engine, the combustion energy has more time to "work" on the eccentric shaft/crank shaft.
As for engine displacement versus turbo, it really has nothing to do with engine displacement.  We're talking about efficient sizing for the engine displacement.  Try and compare identical turbo sizes for piston engine versus rotary engine.  For example...
*Mitsubishi TD-06SH on a rotary engine puts out barely 400 to the wheels.  This same turbo puts out 500 easily on a piston engine (i.e. Toyota 7M-GTE, Nissan SR20).
*Garrett T-66 on a rotary engine will make about 500.  T-66 in a big V8 (Ford 302) will easily make 600.
-Ted
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Originally posted by machinehead
A few things.
One, I personally don't mind an attitude if I am getting something (good reliable information) out of the conversation.
Two, you still need to convert cfm to lb/min if you are going to use the info to read and plot compressor maps. They all show in lbs/min nowadays. But I think you calcualtions are right. I have in my mind something like 300cfm for a stock port 13b.
Anybody know how to convert cfm to lb/min?
A few things.
One, I personally don't mind an attitude if I am getting something (good reliable information) out of the conversation.
Two, you still need to convert cfm to lb/min if you are going to use the info to read and plot compressor maps. They all show in lbs/min nowadays. But I think you calcualtions are right. I have in my mind something like 300cfm for a stock port 13b.
Anybody know how to convert cfm to lb/min?
A rough conversion for CFM to lb/min at ambient is to multiply by 0.069.
That's actually a poor approximation. To do it right you need to include the temperature (PV=nRT) at the intake manifold.
Rearranging, we get n=PV/RT
Formula (using degress Rankine/absolute temp) is:
n (lb/miin) = P (PSI) x CFM x 29/10.73 x DEGR
where P is absolute pressure at sea level (boost in PSI + 14.7), 29 and 10.73 are constants, and DEGR is degrees Rankine (deg F + 460)
Gene
www.purplemantis.com
#37
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Ted.... I'd like to see the answers to your questions since we are ignorant. Especially the meaning of A/R since there are 40 biliion interpretations of it floating around.
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Originally posted by RETed
Please, I'd like to see your proof on this...
-Ted
Please, I'd like to see your proof on this...
-Ted
As I stated in the thread linked above, there is always a compromise. You can easily make over 400rwhp @ 15 psi with a 60-1 compressor. These dynos you see of 350-385rwhp are normally on "standard" street ports (ie. cleaned up rew ports), running .96-1.00 housings. If you run a very LARGE street port (ie. making peak power 8.5-9k) with a 1.24-1.32 housing, I garauntee people would see more than 400rwhp @ 15 psi.
That's generally not the point of the turbo. People pick it because it spools quick.
#39
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Originally posted by Rutt
Ted.... I'd like to see the answers to your questions since we are ignorant. Especially the meaning of A/R since there are 40 biliion interpretations of it floating around.
Ted.... I'd like to see the answers to your questions since we are ignorant. Especially the meaning of A/R since there are 40 biliion interpretations of it floating around.
All I can recommend is get the Hugh MacInness "Turbocharging" and Corky Bell "Maximum Boost" books.  These answer 99% of the questions on turbochargers.
-Ted
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Originally posted by gfelber
Stephen,
The basic formula to calculate engine flow for a turbo application involves a number of factors:
engine displacement, cubic inches (D)
volumetric efficiency (VE)
max RPM (RPM)
displacement/rev (D_R)
conversion factor (1728)
thus:
D x VE x RPM x D_R / 1728
For a nonported rotary:
80 x .70 x 8500 x 1/1728 = 296 CFM (assuming my VE is correct!)
For a 2.6 liter boinger:
160 x .85 x 8500 (yeah right) x 2/1728 = 334
334= 12.5 % greater than the rotary's 296, but there is at least one other factor to consider (below).
Couple of remarks-
A piston engine only displaces half of its volume per revolution, while the rotary displaces all of it's volume per rev. That will change the 13B displcement from 1.3L to 2.6. I think rotary engines have a lower VE than piston engines (and used .7 versus .85), which might explain Ted's 20% estimate.
If this is true, however, then the 20% will diminish if the rotary is ported.
The other factor to consider is exhaust gas temperature which I think is much higher on a rotary compared to a piston engine.
Gene
Stephen,
The basic formula to calculate engine flow for a turbo application involves a number of factors:
engine displacement, cubic inches (D)
volumetric efficiency (VE)
max RPM (RPM)
displacement/rev (D_R)
conversion factor (1728)
thus:
D x VE x RPM x D_R / 1728
For a nonported rotary:
80 x .70 x 8500 x 1/1728 = 296 CFM (assuming my VE is correct!)
For a 2.6 liter boinger:
160 x .85 x 8500 (yeah right) x 2/1728 = 334
334= 12.5 % greater than the rotary's 296, but there is at least one other factor to consider (below).
Couple of remarks-
A piston engine only displaces half of its volume per revolution, while the rotary displaces all of it's volume per rev. That will change the 13B displcement from 1.3L to 2.6. I think rotary engines have a lower VE than piston engines (and used .7 versus .85), which might explain Ted's 20% estimate.
If this is true, however, then the 20% will diminish if the rotary is ported.
The other factor to consider is exhaust gas temperature which I think is much higher on a rotary compared to a piston engine.
Gene
Why is it that in the formula D_R is "1" for the rotary and 2 for the piston??? I'm trying to get a good understanding of this
Thanks,
STEPHEN
#41
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Originally posted by SPOautos
Why is it that in the formula D_R is "1" for the rotary and 2 for the piston??? I'm trying to get a good understanding of this
Why is it that in the formula D_R is "1" for the rotary and 2 for the piston??? I'm trying to get a good understanding of this
What we are trying to figure out is displacement.  For a piston engine, displacement is calculated by piston area X bore.  Now, this "displacement" is "expelled" (as exhaust) or "inhaled" (as intake) ONCE per two revolutions of the crankshaft; this is the definition of a 4-stroke piston engine  Therefore, to extrapolate this equivalent to the rotary engine, we need to take into account what a rotary engine does in two revolutions of the eccentric shaft.  This gets tricky, as you have differing opinions on how this should be considered "equivalent".
Some rotary engine facts...  The rotor, itself, spins 1/3rd the speed of the eccentric shaft.  Therefore, two revolutions of the eccentric shaft only equal 2/3rd's of a revolution of the rotor.  A rotor "swept" volume = 654cc for a 13B.  The front-to-rear rotor relationship is 180&176 out-of-phase; an "adjacent" rotor face front-to-rear is actually only 60° out-of-phase.  To "reference" the eccentric shaft to rotor position, we shall use the front rotor.  Therefore, for two revolutions, the front rotor should spit out 2 rotor faces, which equate to 654cc x 2.  Now, this comes the interesting part - while the front rotor face (RF) is referenced at one apex seal (AS), the rear rotor is in the *middle* of it's exhaust; while the front rotor goes through AS-RF-AS-RF-AS, the rear rotor goes through RF-AS-RF-AS-RF!  This means the rear rotor begins and ends in a middle of an exhaust output.  So how do you count this?
One method - the front is obviously 654 x 2 = 1308cc.  The rear would count as 654 x (0.5 + 1 + 0.5) = 654 x 2 = 1308cc.  Adding front and rear gets you a 2x multiplier of 1308cc as equivalent displacement (2616cc).  This is where the 2.6 liter number probably comes from.
Alternate method - the front is still the same at 654 x 2 = 1308cc.  The rear would count as 654 x (1 + 1 + 1) [how can you get "HALF" an exhaust output?] = 654 x 3 = 2562cc.  Adding front and rear gets you a 2.5x multiplier of 3270cc, which a lot of our piston engine'd racing opponents would love to get the 13B rotary engine bumped up to.
Bottom line, it's hard to get a definite answer to this question, but our original questions is referenced from the first method.
-Ted
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Originally posted by SPOautos
Why is it that in the formula D_R is "1" for the rotary and 2 for the piston??? I'm trying to get a good understanding of this
Thanks,
STEPHEN
Why is it that in the formula D_R is "1" for the rotary and 2 for the piston??? I'm trying to get a good understanding of this
Thanks,
STEPHEN
My bad. Should be .5 for piston and 1 for rotary.
Gene
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Originally posted by blackscorpio
I think with all the discussions on engine displacement we no one is answering the original question t-61 vs T60-1? Which is better unser what application?
I think with all the discussions on engine displacement we no one is answering the original question t-61 vs T60-1? Which is better unser what application?
I was trying to illustrate that one should know VE/displacement before deciding. This will certainly affect turbo selection, particularly for a ported motor versus stock.
Once you do this, take a look at the compressor maps and decide which is best for you, e.g., do you want better spool up, higher peak HP, etc.
Gene
www.purplemantis.com
#45
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The odd shape of the rotary contributes to the fact the rotary has poor THERMAL efficiencies. I think you are all at least a little off on your VE conversations-you need to talk to RiceRacing. (at least clarify the VE to porting etc) One other note VE is not the same for all RPMs!
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Originally posted by spyfish007
The odd shape of the rotary contributes to the fact the rotary has poor THERMAL efficiencies. I think you are all at least a little off on your VE conversations-you need to talk to RiceRacing. (at least clarify the VE to porting etc) One other note VE is not the same for all RPMs!
The odd shape of the rotary contributes to the fact the rotary has poor THERMAL efficiencies. I think you are all at least a little off on your VE conversations-you need to talk to RiceRacing. (at least clarify the VE to porting etc) One other note VE is not the same for all RPMs!
Rice Racing in AU? Can you provide contact info?
Thanks-
Gene
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can you dumb this down a bit (i.e. give some numbers and info without the theory) and use as an example the compressor maps that I linked?
i really just need some info pertaining directly to the turbo applications i listed and then I will go back and sit and figure everything out to make sure i understand it using my application as a pertinent worked out problem/example.
thanks,
Nic
i really just need some info pertaining directly to the turbo applications i listed and then I will go back and sit and figure everything out to make sure i understand it using my application as a pertinent worked out problem/example.
thanks,
Nic
Originally posted by gfelber
Oh yeah
I was trying to illustrate that one should know VE/displacement before deciding. This will certainly affect turbo selection, particularly for a ported motor versus stock.
Once you do this, take a look at the compressor maps and decide which is best for you, e.g., do you want better spool up, higher peak HP, etc.
Gene
www.purplemantis.com
Oh yeah
I was trying to illustrate that one should know VE/displacement before deciding. This will certainly affect turbo selection, particularly for a ported motor versus stock.
Once you do this, take a look at the compressor maps and decide which is best for you, e.g., do you want better spool up, higher peak HP, etc.
Gene
www.purplemantis.com
#48
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gfelber, my remark about attitude was not directed at you, I was defending Ted. And thanks for the formulas.
So if we take your general number of .069 then 300 cfm becomes about 20lbs/min. double that for running 15 psi of boost and we get 40lb/min which is right in the peak efficiency range of the 60-1 with some room to spare. So basically unless you are going to run 30psi then the 60-1 is a good compressor for the 13b. Its good on paper and in real life, which is probably why it is so popular.
What I can't see however are any drawbacks to the T61, other than the price. It seems like it will do everything the 60-1 will do but it will also allow you to run higher pressure levels if you want.
So if we take your general number of .069 then 300 cfm becomes about 20lbs/min. double that for running 15 psi of boost and we get 40lb/min which is right in the peak efficiency range of the 60-1 with some room to spare. So basically unless you are going to run 30psi then the 60-1 is a good compressor for the 13b. Its good on paper and in real life, which is probably why it is so popular.
What I can't see however are any drawbacks to the T61, other than the price. It seems like it will do everything the 60-1 will do but it will also allow you to run higher pressure levels if you want.
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Spyfish beat me to part of my intended response, but what also I was going to add is that extended overlap of the engine will increase the general CFM intake of the engine..
Although the calculations are rather sexy seldom do they hold water in the real world, even on a 13b na I have measured over 350 cfm moving through the intake tract...
To compensate for overlap and wasted inlet charge, the VE should actually be increased over 100%, not decreased..Max
Although the calculations are rather sexy seldom do they hold water in the real world, even on a 13b na I have measured over 350 cfm moving through the intake tract...
To compensate for overlap and wasted inlet charge, the VE should actually be increased over 100%, not decreased..Max
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It can be done
Pertaining to the actual topic of the the thread:
Ok, for starters, here is Brian Cains dyno. He is running a 60-1 hifi with a .96 undivided hot side with an undivided cast iron manifold and an air to water intercooler which is VERY effecient... (just like ted said several posts back, but I thought I would reiterate). This run was made at 17psi and obtained 424 rwhp:
Now, I know for a fact that Don Marvel made a 13B-rew with a 60-1 (with a small A/R) make 435 rwhp at 4500 rpms, but it died off after that and ended up making about 390 at 8000 rpm. They changed the compressor wheel to a 63 series and was able to get in the 480 rwhp area, but I don't know the exact number or rpm, but I would estimate 5200 rpm.
That same engine, when switched to run alcohold, ended up putting out 519rwhp at (I'm trying to remember the RPM here, I know I have the hp right) 6000 rpm.
Maybe your engine builders just don't know how to port for the turbo you are going to be using.... Don is able to take a turbo, its specs, and somehow design a port configuration and style in his head that will optimize EVERYTHING for the car... these ports were made for a lower A/R (I think it went on a sand rail... but I may be wrong here).
You want power and range like you stated, you need to get in contact with a god of rotaries like Marvel.
Ok, for starters, here is Brian Cains dyno. He is running a 60-1 hifi with a .96 undivided hot side with an undivided cast iron manifold and an air to water intercooler which is VERY effecient... (just like ted said several posts back, but I thought I would reiterate). This run was made at 17psi and obtained 424 rwhp:
Now, I know for a fact that Don Marvel made a 13B-rew with a 60-1 (with a small A/R) make 435 rwhp at 4500 rpms, but it died off after that and ended up making about 390 at 8000 rpm. They changed the compressor wheel to a 63 series and was able to get in the 480 rwhp area, but I don't know the exact number or rpm, but I would estimate 5200 rpm.
That same engine, when switched to run alcohold, ended up putting out 519rwhp at (I'm trying to remember the RPM here, I know I have the hp right) 6000 rpm.
Maybe your engine builders just don't know how to port for the turbo you are going to be using.... Don is able to take a turbo, its specs, and somehow design a port configuration and style in his head that will optimize EVERYTHING for the car... these ports were made for a lower A/R (I think it went on a sand rail... but I may be wrong here).
You want power and range like you stated, you need to get in contact with a god of rotaries like Marvel.
Last edited by Kurgan; 06-13-02 at 12:22 AM.