ideal compression on an m20 stroker with custom pistons
Posted: Jun 11, 2012 11:11 PM
I know this is not an e30 site, but my brother thought you guys could throw me some knowledge on my choice, so I am using his profile to post and thus my problem and my possible solutions.
I am rebuilding an m20 right now, it came with Ross Racing forged pistons and rods after the previos owner snapped the timing belt. Ultimtely I would like to turbo this engine and thus am stuck deciding on a compression ratio and the necessary parts to make that happen.
The pistons I have are meant for an m20b30 by using the s52 crank (89.6mm) however I pulled it apart due to the low compression numbers I was seeing and found out it still has the stock 76mm crank in it. With this setup the compression ratio would be ~9.75:1 and 2979 cc. (the numbers I am seeing are about 6:1 with the crankshaft I have in it!!) With a turbo down the road I know this is not ideal with the likelihood of detonation under boost.
I also looked at the s50 crank (86mm) and am considering this as an option. This would resultin 2860cc displacement and a compression ratio of ~8.1:1. The head is stock as of now and I know the 745i turbo had a 7 or 8:1 compression ratio and this could be a good range for it. The interesting twist is that I am a mile high above sea level. I have been looking at low boost applications and am tentatively planning the rrfpr and chip method-- please do not turn this into a which fuel management method is better argument.
I compared a low boost stock m20b25 setup with 8 psi at sea level to both of the setups i am looking at right now. The results surprised me and got me to thinking, here is the link to the stock setup:
http://www.zealautowerks.com/index.html ... 0,6500,0,8
As you can see the stock compression ratio of 8.8:1 yields an effective compression ratio of 13.6:1. It is safe to say this is the limit on the stock motronic fuel system with a chip, many builds have used this method with a rrfpr. Remember this is a 2.5L engine.
I then punched in the ross racing setup with the same 8 psi but at an altitude of 5000 feet (Denver is 5280', I am around 6500' in Colorado Springs). This would be a 3.0L engine.
http://www.zealautowerks.com/index.html ... 500,5000,8
These results surprised me because the 9.75:1 Ross Racing Setup yielded an effective compression ratio of 8.78:1 at 5000' and an effective compression ratio of 13.56:1 under 8 psi of boost at 5000'. This means I would be seeing the same power at altitude as a stock m20 would be seeing at sea level.
The other option with the s50 crank would yield lower results.
http://www.zealautowerks.com/index.html ... 500,5000,8
The compression ratio would be lowered to a lesss than impressive ~8.1:1 in a 2.86L engine. Remember the 745i turbo had 7:1 or 8:1 compression out of a 3.5L engine. One 8 psi this engine would effectively be 11.06:1. This would leave room to up the boost but fuel management would need to changed to accomodate.
So what do you think? I am seriously considering the 89.6mm crank as it should be ideal and would maximize performance without including additional management costs. Of course this setup would need some sort of sea level valve that is opened below 5000' to keep detonation from occuring and have maybe 1 psi of boost.
What are your thoughts on the shorter 86mm crank and resulting compression ratio? We could get into porting of the head and cams as well but for now assume the head is stock and the same for all applications, the difference is solely the crank and resulting compression ratio.
I am rebuilding an m20 right now, it came with Ross Racing forged pistons and rods after the previos owner snapped the timing belt. Ultimtely I would like to turbo this engine and thus am stuck deciding on a compression ratio and the necessary parts to make that happen.
The pistons I have are meant for an m20b30 by using the s52 crank (89.6mm) however I pulled it apart due to the low compression numbers I was seeing and found out it still has the stock 76mm crank in it. With this setup the compression ratio would be ~9.75:1 and 2979 cc. (the numbers I am seeing are about 6:1 with the crankshaft I have in it!!) With a turbo down the road I know this is not ideal with the likelihood of detonation under boost.
I also looked at the s50 crank (86mm) and am considering this as an option. This would resultin 2860cc displacement and a compression ratio of ~8.1:1. The head is stock as of now and I know the 745i turbo had a 7 or 8:1 compression ratio and this could be a good range for it. The interesting twist is that I am a mile high above sea level. I have been looking at low boost applications and am tentatively planning the rrfpr and chip method-- please do not turn this into a which fuel management method is better argument.
I compared a low boost stock m20b25 setup with 8 psi at sea level to both of the setups i am looking at right now. The results surprised me and got me to thinking, here is the link to the stock setup:
http://www.zealautowerks.com/index.html ... 0,6500,0,8
As you can see the stock compression ratio of 8.8:1 yields an effective compression ratio of 13.6:1. It is safe to say this is the limit on the stock motronic fuel system with a chip, many builds have used this method with a rrfpr. Remember this is a 2.5L engine.
I then punched in the ross racing setup with the same 8 psi but at an altitude of 5000 feet (Denver is 5280', I am around 6500' in Colorado Springs). This would be a 3.0L engine.
http://www.zealautowerks.com/index.html ... 500,5000,8
These results surprised me because the 9.75:1 Ross Racing Setup yielded an effective compression ratio of 8.78:1 at 5000' and an effective compression ratio of 13.56:1 under 8 psi of boost at 5000'. This means I would be seeing the same power at altitude as a stock m20 would be seeing at sea level.
The other option with the s50 crank would yield lower results.
http://www.zealautowerks.com/index.html ... 500,5000,8
The compression ratio would be lowered to a lesss than impressive ~8.1:1 in a 2.86L engine. Remember the 745i turbo had 7:1 or 8:1 compression out of a 3.5L engine. One 8 psi this engine would effectively be 11.06:1. This would leave room to up the boost but fuel management would need to changed to accomodate.
So what do you think? I am seriously considering the 89.6mm crank as it should be ideal and would maximize performance without including additional management costs. Of course this setup would need some sort of sea level valve that is opened below 5000' to keep detonation from occuring and have maybe 1 psi of boost.
What are your thoughts on the shorter 86mm crank and resulting compression ratio? We could get into porting of the head and cams as well but for now assume the head is stock and the same for all applications, the difference is solely the crank and resulting compression ratio.