To summarize, I have a preexisting compressor and data from another student. I noticed the blade profile does not look accurate, but I have a feeling it could be more than that. I am solving for pressure at the outlet of the first stage so we can spec a sensor on our test cell. I give AxMAP mass flow rate and have all mandatory fields filled out plus most or all input fields. I get bad calculations and am hoping I can get some help finding out what the reason for the bad calculation is.