|Feb18-11, 05:28 PM||#1|
Static pressure in Compressor, Burner, Turbine
I posted a question about this a couple days ago but I have since solved for the total temperatures in the compressor, burner, and turbine.
My question is this. How do I calculate the static pressure in the compressor, burner, and turbine when i know the following data at each station?
speed of sound
mass flow rate
I need to know the static temperature so I can calculate the density, which then leads to calculating the area.
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