Okay, let's see if I can figure this out here. Say for our example, the engine is operating at 3500 RPM, is a 3100 cubic centimeter engine, has an intake manifold pressure of 20 pounds per square inch, with an intake charge temperature of 70 degrees. We'll say we're at sea level, for an atmospheric pressure of 14.7 psi.
So our variables (constants) are as follows:
Displacement = 3100cc = .0031 cubic meters
Engine Speed = 3500 RPM
P = 20 PSIg = 34.7 PSIa = 239.2 kPa
T = 70*F = 21.1*C = 294.3*K
Each rotation displaces 3100 cubic centimeters of (atmospheric pressure) air divided by two, as there is only one intake stroke every other revolution. Using our constants, we can find the number of moles of air.
PV=NRT
(239.2 kPa)(3.1x10^-3 cubic meters)(1/2) = n (8.314 J*K^−1*mol^−1)(294.3 K)
Solving for n using a TI-89 because I don't wanna deal with that bullshit gives us:
n=0.171079881880499 moles of air per full revolution.
(0.171079881880499 moles/revolution)(3500 revolution/minute) = 598.779586582 moles/minute of airflow (instantaneously)
Our target AFR is 11.5 to 1. At STP, 1 mole of gasoline occupies 22.4L. This means we need (598.779586582 moles per minute)/11.5 = 52.07 moles per minute of fuel to obtain it. This translates to 1166.368 cc/min of gasoline at this instant.
Does anyone see any flaw with this math? There is a reason for wanting to know this :-P Discuss.



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Let me revise.

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