03. Gas turbine engines in aircraft, also called jet engines consists of compressor to increase the pressure of the incoming air before it enters the combustor. (2 pts) Process Engineer Garrett proposes to replace the single-stage compressor with a multistage compressor (see figure below) for the process. Help him prepare a P-V diagram for the process as part of his report to the Process Head Macy. (0.5 XC) Will the proposed process end up saving work done? Help Process Head Macy convince profit minded Plant Head/Manager Pearson. (Hint: Provide a comparison between single- and multi-stage compressors) Compressor 1 Compressor 2 w Intercooler Postcooler M wsro