Squirrel:
You don’t furnish much basic data, such as:
Is your gas pure, or a mixture? Is it dry or wet?
What are your suction and discharge conditions?
Is your compressor a recip or a centrifugal?
Is your compressor a single stage – or multi-stage?
What do you define as “Max accuracy”?
What EOS are you using? What simulator?
As Pmover and David have done, I can only address your concern in generalities – but I can add some experienced advice:
By “sizing” I assume you are calculating the adiabatic head / horsepower requirements, and discharge temperatures;
As Pmover infers, leave the rest of the “design” to the proven experts – the compressor’s manufacturer;
Refer to Royce N. Brown’s book, “Compressors - Selection and Sizing”; 2nd Edition; Gulf Professional Publishing. Read the section titled “Real Gas Exponent”. Even Brown fails to explicitly go into the details of finding and applying specific heats of gases in compressor calculations. However, he at least does mention some of the important details left out of most academic Thermodynamic text books.
Understand and accept the fact that the relationship
MCp - MCv = R = 1.986 Btu / (lbmol - °F)
Is a purely theoretical one based on “ideal” gas conditions – which are not realistic and unavailable in the real world. The same facts apply to the specific heat ratio derived from it. Reflect on the definition of ideal gas conditions: 1.0 atmospheric pressure and approximately 70 oF. Even if you are fortunate to calculate an accurate specific heat value for an ideal gas, what do you do with it when your compression conditions are probably various atmospheres of pressure and your average stage compression temperature is around 150 -160 of?
Accept the fact that the specific heat at constant pressure is NOT A CONSTANT – nor is the Cv. Also accept the fact that both gas specific heats will be varying from the suction port to the discharge port on the compressor in question – and you have no way to calculate that path, except to estimate it. Most manufacturers – including myself – have tried to identify the specific values at suction and discharge and then simply averaged them to obtain the “realistic” k that can then be used in the applicable equations to calculate, for example, the discharge temperature. This has been a sore subject with me for the past 50 years as I have not yet found or heard of a Thermodynamic paper dealing and explaining this fact as it relates to compressor calculations. I have found that University profs and text book authors simply prefer to avoid this subject.
As the GPSA has always stated – and even Brown also – use Mollier diagrams (in the case of pure gases) to obtain the maximum in accurate compressor calculations. Mollier diagrams are derived from reliable EOS, so an accurate and proven EOS will also work – as David also suggests.
Some gases - such as ethylene - can be mavericks, varying in specific heat values in strange ways without any respect for the academic relationship predicted by academics.
I hope these comments are of some help to you.