a) Given that for a flew process the steady flow equation is: q-w=\left(u_{2}-u_{1}\right)+\left(p_{2} v_{2}-P_{1} v_{1}\right)+\left(\frac{C^{2}}{2}-\frac{C_{1}^{2}}{2}\right)+p\left(x_{2}-z_{1}\right) b) Explain how the following jet engine works. Refer to each section of the engine

and explain the purpose of each section. e) Draw a Temperature (T) versus Entropy (s) diagram for a typical gas turbine. The diagram should show the processes for an actual gas turbine and should show the effect of real world losses where the compressor and turbine have an isentropic efficiency and pressure losses in the combustion chamber in an actual gas turbine.Explain each of the processes on the T-s diagram.