Consider the engine shown below . This is a two-spool turbofan engine with turbine cooling bleed air, a fan mixer , and an afterburner . The...

I need to know how to draw t-s diagram,

I need right answers as many as possible to compare to mine.

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Consider the engine shown below . This is a two-spool turbofan engine with turbine cooling bleed air,a fan mixer , and an afterburner . The high-pressure turbine ( HPT ) drives the compressor and the low -pressure turbine ILPT) drives the fan . Bleed air is extracted after the compressor and can beconsidered to be mixed back in after the flow leaves the high- pressure turbine . The flow exiting the(17 pts )LPT is mixed with the fan flow before it enters the afterburner ( this is different than in your project ) .A partially complete I - 5 diagram for the engine ( from a to 5 m ) also is given below .2 ) Add the following labels to the I - 5 diagram : a , 09 , 01 , 02 , 03 8 , 03 , 04, 051, 051', 052, 05 m.Connect the dots along the path of the main flow through the engine core from Da to 05 72 15.5pts )b ) Draw lines indicated curves at constant Post , Poz , and POSI . (2.5 pts )C ) Complete the diagram by including points 06 , De , and e with JOE > To, and we > U / U is theflight velocity ) ( 3 pts )d) From the enthalpy balance over the afterburner , determine the function 9 , such thatTOG = 9 (f , Jab , B, Cp5m . ( PG , Tosm. nab, Or )where f = my / Man , fab = me. ab / man , nab is the afterburner combustion efficiency , and Q , isthe heat release per unit mass of fuel . State any assumptions . ( 6 pts )( 1 + B ) maHBMmall34