Cooling method for gas turbines

Cooling method for gas turbines. Refer to the Journal of Engineering for Gas Turbines and Power (January 2005) study of a high-pressure inlet fogging method for a gas turbine engine, Exercise 4.13 (p.188).  Recall that you fit a first-order model for heat rate (y) as a function of speed, inlet temperature, exhaust temperature, cycle pressure ratio, and air flow rate, to data saved in the GASTURBINE file.

No solution has been posted yet. You have opportunity make $10!