matlab turbojet populsions problem

Project Description:

walk through the different stages in a turbojet engine (inlet/diffuser, compressor, combuster, turbine, nozzle, augmenter/afterburner) to determine specific thrust, tsfc, efficiencies (thermal, propulsive, and overall), make plots, and include code. please see attached for details. need completed product by 8:00 am tomorrow morning.
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Project Stats: Edited

Price Type: Fixed

Project Budget: $50 to $100
Total Proposals: 3
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