Axial flow compressor

About this project

I am developing low power axial flow compressor. It will be used in jet engine. Goal is to have 20 cm inner diameter of compressor, 15 stages, shaft diameter is 2cm and drum diameter is 3cm on the first stage up to 19.355 cm on the last stage. Goal axial velocity is 97,692 m/s and pressure ratio is 15,4. Casing inner diameter is constant throughout whole compressor. If you need any other specifications, please contact me.