Bristell NG-5 Propulsion System Engineering

The assignment involves analysing and designing a propeller propulsion system for a Bristell NG-5 aircraft. There are three main tasks: Propeller Design: Use Blade Element Momentum Theory (BEMT) to calculate propeller performance, using real aerofoil data, and conduct sensitivity analysis and experimental validation. Engine Analysis: Perform thermodynamic calculations to determine engine power and fuel consumption (BSFC) at sea level and different altitudes, and compare results with existing aircraft engines. Engine–Propeller Matching: Determine the optimal propeller diameter, number of blades, blade pitch distribution, and RPM settings for climbing and cruising while minimising fuel consumption. Required deliverables: A professional engineering report (maximum 8 pages, excluding front matter, references and appendices). MATLAB codes for all calculations, simulations and graphs, submitted in a ZIP file. Engineering calculations, graphs, validation and academic references. I have the assignment instructions, a MATLAB BEMT starter code and a draft report available. I need someone experienced in MATLAB and aerospace propulsion engineering to help verify the calculations, correct the code and finalise the report according to the assignment requirements.