What is an Adiabatic Expansion Coefficient?

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SUMMARY

The adiabatic expansion coefficient, denoted as γ (gamma), is crucial for calculating the performance of air compressors. In this discussion, users explored its significance in relation to an air compressor calculator, specifically for a single-stage compression scenario with initial and final pressures of 14.5 psi and 100 psi, respectively. The commonly accepted value for air is 1.4, representing the ratio of specific heats. However, discrepancies arose when calculating horsepower, suggesting that the calculator may not account for the significant temperature rise during compression, which can lead to much higher final pressures than estimated.

PREREQUISITES
  • Understanding of adiabatic processes in thermodynamics
  • Familiarity with the concept of specific heats and their ratios
  • Knowledge of air compressor operation and performance metrics
  • Basic skills in using online engineering calculators
NEXT STEPS
  • Research the implications of temperature rise in adiabatic compression
  • Learn about the polytropic process and its equations
  • Investigate alternative air compressor calculators that account for thermal effects
  • Study the relationship between horsepower and pressure in compressed air systems
USEFUL FOR

Engineers, HVAC professionals, and anyone involved in the design or operation of air compression systems will benefit from this discussion, particularly those seeking to optimize performance calculations.

Natla
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Hi,

Can anyone tell me what this means?

I'm trying to find the adiabatic expansion coefficient in order to use this air compressor calculator.

http://www.engineeringtoolbox.com/horsepower-compressed-air-d_1363.html

These are the variables I have at the moment...

Number of stages- 1

absolute initial pressure (psi)- 14.5

volume of compressed air at atmospheric pressure (cfm)- 20

absolute final pressure (psi)- 100.

So what is this adiabatic expansion coefficient and how can I calculate for it?

Thanks.
 
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I'm not absolutely sure, but it looks like they're using the ratio of specific heats. Actually, it's the exponent in the polytropic equation, but for a perfectly isentropic process, the exponent becomes the ratio of specific heats. For air, use 1.4
 
Hi,

Thanks so much for your help.
 
On second thought. Perhaps 1.41 is not correct. Becuse then the calculation just doesn't seem correct, it doesn't take not nearly enough horsepower.

I don't think that this calculator considers the rise in temperature of the compressed gas. I mean I made it calculate for 7cfm at 14.5 psi to compress to 1,450 psi. Thats a compression in a single stage to a factor of 100. So, the rise in temperature for this compressed gas would be about 1,500 degress celsius.

This would bring the actual final pressure to about 14,500 psi. And it's trying to say that the compressor would only be rated at 4.29 HP. That isn't right.

So what else could it be?

Thanks.
 

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