You are confused. Compression ratio is the cylinder volume of BDC to TDC. This ratio effects efficiency, not "effectiveness."
Boost is the measure of increase over atmospheric pressure. It doesn't change volumetric compression ratio. As it changes charge density and not physical volume on either end of the stroke/cycle.
Compression pressure is both the geometric and manifold pressure, this means that both the geometric and atmospheric compression ratios combine to arrive at the cylinder pressure at TDC. Which means there is an effective compression ratio. Compression ratio is compression ratio, it has nothing to do with efficiency and everything to do with the compression of the air.
It doesn't change volumetric compression ratio.
I know, I said that, but the density increase increases the effective cylinder pressure, in the same way that the piston itself increases the cylinder pressure as it moves to TDC. So what then becomes the effective compression ratio when boost is factored in? With an axial jet engine the compression ratio is straight forward, the pressure tap reads 147psi at the end of the second spool compressor, that's a 10:1 compression ratio.
With a piston engine, you have volumetric compression of the air in the cylinder and density compression with the turbo. Both are physically compressing the air at a certain ratio, the two events do not exist in isolation, and combine to produce an effective cylinder pressure.
the pressure tap is psia?
It can be.
Ask what you're trying to accomplish. Because you're stating things which are incorrect and asserting I'm the one in error.
What part is incorrect? What I'm trying to accomplish is stated in the OP.
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