Axial gas compressor (from a turbine)

Description

Was my undergrate thesis, compressor of a turbine siemens SGT 6 8000H design using the methods of Cohen book and excel to do the calc; All of the inlet parameters i got from the Siemens Website https://www.siemens-energy.com/global/en/offerings/power-generation/gas-turbines/sgt6-8000h.html After the calculation of all the angles, i did the design using Ansys bladegen and SpaceClaim.