Back in 1978, I wrote in my CL Racing column in Model Aviation:
A good question to ask here is, "How much does
this pressure change affect the total pressure in at
pressure system?" In order to find an answer to this,
you have to know the pressure that is created in the
tank by using crankcase pressure. I set up
a test stand to measure this and found that the tank
pressure from an untimed crankcase tap is about 1.4
psi, or about 1.6 psi if a ball-check is used in the
pressure line.
The entire column can be seen at http://www.nclra.org/TechTopics/UniflowPhysics.pdf (http://www.nclra.org/TechTopics/UniflowPhysics.pdf)