Correct me if I'm wrong but at 12:1 you'll have to run higher octane than what you're getting from the pump
There are three different compression ratios in an engine:
1. Static compression
2. Dynamic compression
3. Effective compression
Static compression is the actual measured volumes.
Dynamic compression is loosly based on static compression, but uses the closing point of the intake valve as the stroke to calculate the volume above the piston. This is a function of the stroke, rod length, and the degrees after Bottom Dead Center (BDC) that the intake valve closes. This is because air can not be compressed until it is confirmed. Basically, a larger cam requires more static compression to produce the same cylinder pressure.
Effective compression is what the engine actually experiences while running. It is a product of dynamic compression ratio and volumetric efficiency (VE). Good flowing intake and exhaust systems promote higher VE, restrictive ports or overly large (lazy) ports with low velocity can reduce VE, as ca the operating environment.
Check out these other threads for additional information:
Another cam question bbc
http://www.socaljetboats.com/index.php?topic=23935.msg278726.msg#278726How to choose the right octane?
http://www.socaljetboats.com/index.php?topic=23425.msg271550.msg#271550VE changes throughout the RPM range with peak VE being at peak torque RPM. For every VE, the dynamic compression will compress the air/fuel mixture X amount with a corresponding increase in temperature. This change in temperature is added to the Intake Air Temperature (IAT). Heat is always conducted from areas of high temperature to areas of low temperature. Combustion chamber heat can be lost or gained by conduction through the cylinder walls, piston domes, combustion chambers in the heads, valves, head gaskets, or any surface that is in contact with the air/fuel mixture that I might have forgotten. In the event of supercharging, the turbo or blower heat the air in its own right in which case, this number is added to the sum above. If this number is greater than the flash point of the fuel, prior to ignition, detonation will occur.
Then there is the matter of mixture motion inside the combustion chamber. A highly turbulent mixture is homogenous and burns evenly. Fuel droplets fall out of suspension and/or from large droplets that do not burn evenly.
Here is a good article by Jim McFarland on burn patterns:
http://www.hotrod.com/how-to/engine/ctrp-1108-combustion-patterns/A good article on compression ratio by Da Viz:
http://www.hotrod.com/events/coverage/0311em-power-squeeze/