NASA NTRS · 20000110100
Adiabatic Compression of Oxygen: Real Fluid Temperatures
Abstract
The adiabatic compression of oxygen has been identified as an ignition source for systems operating in enriched oxygen atmospheres. Current practice is to evaluate the temperature rise on compression by treating oxygen as an ideal gas with constant heat capacity. This paper establishes the appropriate thermodynamic analysis for the common occurrence of adiabatic compression of oxygen and in the process defines a satisfactory equation of state (EOS) for oxygen. It uses that EOS to model adiabatic compression as isentropic compression and calculates final temperatures for this system using current approaches for comparison.
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Barragan, Michelle, Wilson, D. Bruce, Stoltzfus, Joel M.. 2000-01-01. Adiabatic Compression of Oxygen: Real Fluid Temperatures. https://ntrs.nasa.gov/citations/20000110100
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