roldy
Feb18-11, 05:28 PM
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?
Known:
Mach #
Static Temperature
Total Pressure
Static Temperature
speed of sound
velocity
mass flow rate
I need to know the static temperature so I can calculate the density, which then leads to calculating the area.
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?
Known:
Mach #
Static Temperature
Total Pressure
Static Temperature
speed of sound
velocity
mass flow rate
I need to know the static temperature so I can calculate the density, which then leads to calculating the area.