(Solved): Need help with a Gas turbine design project. the gas turbine cycle I have pictured is the one I crea ...

Project for Gas Turbines - Project II You work for a gas turbine design company and have a client who has a fairly loose specification for a new gas turbine engine getting designed. You are required to design an aviation gas turbine to power the aircraft with minimum efficiency requirements of \( 40 \% \). Though the client wants to achieve lowest fuel consumption possible. The following guideline efficiencies have been given to assist in the design process. You have total discretion to assume the temperatures, pressures and any other variable you deem necessary unless stated above, though assumptions need to be of sensible values that are justified given current engineering technology. Your brief summary report should include as a minimum the following; 1- Discuss selection of different components and types. You need to demonstrate why a particular type/component or value has been selected as compared to others. Your answers could have both numerical and theoretical response to this part. 2. What are outlet pressures and temperatures 3. Show calculations of work transfer from turbine to compressor, rest calculations are not needed. Your submission should not exceed 3 pages of \( A 4 \) including all text, equations. Use font size 12 and line spacing 1. If helps, Students can write equations and draw diagrams by hand and place them in the submission.