For an open type - Brayton cycle with perfect regeneration: Tmin = 27 oC, rp = 9, plow = 1 bar, Tmax = 1327 oC, Tflame =2000 K, nis,t = 85%, nis,c = 75%. 1. Perform first and second law analysis on each component of the cycle and the whole cycle as well. 2. Show the effect of changing the efficiency of the compressor, from 60% to 100%, on the overall performance of the cycle with respect to the first and the second laws of thermodynamics. 3. Show the effect of changing the efficiency of the turbine, from 60% to 100%, on the overall performance of the cycle with respect to the first and the second laws of thermodynamics. 4. Show the effect of changing Tmax, from 1000 oC to 1500 oC, on the overall performance of the cycle with respect to the first and the second laws of thermodynamics. 5. Show the effect of changing Tmin, from 0 oC to 50 oC, on the overall performance of the cycle with respect to the first and the second laws of thermodynamics. 6. Show the effect of changing the regeneration efficiency, effectiveness (), from 60% to 100%, on the overall performance of the cycle with respect to the first and the second laws of thermodynamics. Represent your results in the form of graphs/plots showing the relationship between the performance factors (power - thermal efficiency - exergy loss - entropy generation - second law efficiency) and the variables the effect if changing the turbine and compressor efficiency from 60% to 100% on overall preformance