BigInch:
What I'm trying to do is teach a group of civil engineers how to select a blower/compressor. Unfortunately, the curriculum for civil engineers covers only incompressible fluid dynamics and a bare minimum of thermodynmics. When you start talking density changes with compressible flow and adiabatic versus polytropic they get lost very quickly.
For the most part these compressors handle atmospheric air with ambient inlet conditions and the discharge pressure is generally less than 10 pounds. Therefore, I'm not concerned about compressibility effects and, for the temperatures and pressures I'm looking at, air behaves as an ideal gas.
If I can get a curve of pounds of air (not CFM) versus discharge pressue, then I've taken density out of the equation. A pound of air is a pound of air, but the volume it occupies is quite different.
What I'm struggling with is, if you consider a discrete molecule of gas, the centrifugal impeller is going to accelerate that molecule to a specific velocity based on the inlet and outlet curvature angles and the rotative speed of the impeller. I beleive that that velocity is a unique value and it is independant of the weight of the molecule because Avogodro says that there is an equal number of molecules in a fixed volume of gas or gas mixture (molecules in has to equal molecules out). The pressure rise is a direct function of the molecular weight of the gas molecule and the square of the discharge velocity. If this is true, then there should be a single unique curve for that impeller when it handles a gas of a known molecular weight.
What am I missing here?
Bduane