please answer one of the following requirements with a solution not an explanation for either a Boeing-737 (CFM56-7B) or Airbus A320 (CFM56-5B)

Design a two stream Un-boosted turbofan engine with a specified OPR, TIT and BPR, for the optimum FPR. 1. Construct carpet plot, specific thrust (F/m) versus specific fuel consumption (SFC) at different OPR(c), and turbine inlet temperature TIT (Tt4) 2. Choose the design parameters (c,Tt4,F,). 3. Choose a designed Aircraft, calculate the engine sizing ( m,A1,AB,A18 ) based on the required thrust for straight and level flight using twin turbofan engines, if needed you can assume the airplane drag polar CD=0.03+0.3CL2