Cam I going to use is 23-223-4, Comp Cams XE268H, which has ABDC of 60. Not sure if that helps.
I believe Comp Cams use 0.006" lobe lift for their "advertised" duration (268 degrees) with hydraulic lifter cams?
I like using the 0.006" lobe lift numbers for comparing Dynamic Compression ratio. "Dynamic" is not really a good description of the ratio number, I usually call it "Effective" compression ratio.
It is just a static compression ratio re-calculated from the closing point of the Intake valve. Normally used to estimate the cranking cylinder pressure.
The intake closing point can also be changed by advancing or retarding the cams installed centerline.
The basic idea is starting at the installed centerline of the cam (106 degrees) which normally splits the cams duration in half, assuming symmetrical open and closing sides of the lobe (268/2 = closing point 134 degrees past the cams installed centerline), so add the centerline 106 plus half lobe duration to closing point 160+134=240 degrees after TDC. But the closing point is normally listed as after BDC, so subtract 1/2 a circle (180 degrees) and 240-180 = 60 degrees after BDC.
The piston position when the valve closes is used to re-calculate the "compression" stroke length.
The math is a bit more complex, but it really boils down to the piston position due to crank rotation "and" the angle the connection rod makes between the piston and crank throw.
We want the piston position after BDC when the intake closes, so we need the distance the crank moved up from bottom dead center, which is just the Cosine of 60 degrees = 0.5 (intake closing point) times 1/2 the crank stroke 3.75" / 2=1.875" (Radius of rotation), so the crank position is only 0.9375" above BDC
For a Spread Sheet calculation: Crank Vertical offset =(STROKE/2) * (COS(INTAKE CLOSING DEGREES * PI() / 180)) = 0.938"
With our 6.768" long rod, we need to know how much the rod is moved over to the side and tilted keeping the piston down a bit lower in the cylinder. Assuming the piston pin is centered (if the pin is offset, then the offset would need to be added or subtracted), anyhow, the crank pin side to side position is just Sine of 60 degrees = 0.8660... again multiplied by crank radius (1/2 stroke = 1.875"), so the rod is moved over from the center by 1.6238" .
For a Spread Sheet calculation: Crank horizontal offset =(STROKE/2) * (SIN(INTAKE CLOSING DEGREES * PI() / 180)) = 1.624"
Just using Pythagorean theorem, this gives the new height above the crank with a known rod length.
Starting with our 6.768" length rod, take the square root of the rod length ^2 - the Crank horizontal offset ^2 = 6.6633" (compared to the full 6.768" at TDC/BDC)
For a Spread Sheet calculation: Piston height due to rod tilt =SQRT((ROD LENGTH ^2)-(Crank horizontal offset)^2)) = 6.663"
Now you have the information to find the piston position ABDC when the intake closes.
There are several ways to put these together depending on what your reference position is, but I just want the new compression (not stroke) length that I can drop into a static compression ratio calculation.
I take the piston position as the crank Vertical offset = 0.938" minus the difference in height due to rod tilt (Original Rod Length - Rod height with tilt) 6.768 - 6.6633 = 0.10470" height diff due to rod tilt. Subtract from crank vertical height change 0.938" - 0.1047" = 0.8328" piston position above BDC at intake closing.
Then to get the compression distance = STROKE - Piston Position, 3.75 - 0.8328 = 2.9172"
Calculating the new Effective compression ratio, if you started out with a 10:1 static compression ratio 440, The Effective (Dynamic) compression with this cam would be 8:1 compression.
Using the pressure formula that was in the Panic Tech Papers @
http://victorylibrary/mopar/cam-tech-c.htm, you just take the Effective compression ratio and rise it to power of 1.2 (the 1.2 number was used, and seems OK for comparison sake. It would vary depending on the sealing and thermal dynamics of the engine.) then multiply that number by your atmosphere air pressure 14.7 at sea-level std temp.
so 8^1.2 = 12.13 * 14.7psi = 178.25 psi Absolute pressure. with a gauge reference pressure to atmosphere (14.7) so Gauge pressure is 178.25 - 14.7 = 163.55 psi approximate cranking cylinder pressure at sea-level, ect, ect....