Create a Matlab script to determine the compressor exit temperature and pressure, the turbine exit temperature and pressure, the nozzle exit Mach number for a real single spool turbojet engine (with losses) with the input data tabulated in Table 1 for three M, conditions. T4 Mo 0.8, 1, 1.2 7c = 9 Po = 29.92 kPa To=229 K Cpe 1.004 kJ/(kgK) Cpt = 1.239 kJ/(kgK) 7b = 0.99 Tdmax = 0.95 = Tb=0.905 Po/P=0.8 1750 K hPR = 42800 kJ/kg Yt=1.3 Ye=1.4 ee = 0.85 7m=0.98 = 0.89 Tn = 0.98 Matlab script should read the data, locate the T and/or f based on user input, and perform the interpolation and/or iteration if needed. Thus, the script should be applicable to any user input for a single spool turbojet (without afterburner). All iterations should continue until the change between the two successive results is less than 0.0001. With a separate script, create four plots: Mo variation vs e Mo variation vs , Mo variation vs T5, Mo variation vs Mg. Briefly discuss your plots with an emphasis on the influence of Mo variation on et, Tis and Mo