Feb18-11, 06:28 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?
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.
|Register to reply|
|Turbine and compressor maps||Mechanical Engineering||4|
|Compressor and turbine design||Mechanical Engineering||4|
|how we increase the pressure of a air compressor||Engineering Systems & Design||4|
|Compressor As a Steam Turbine||Mechanical Engineering||4|
|gas turbine burner pressure||Mechanical Engineering||9|