Engine Simulation performs design point analysis of gas turbine engines such as turbojet turbofan and turboprop. By receiving input values from the user it calculates important performance parameters of gas turbine engines such as:

★ Specific Thrust
★ Thrust Specific Fuel Consumption
★ Thermal Propulsive & Overall Efficiencies.

It also features options to use an Afterburner and Convergent or Convergent-Divergent Nozzle in the Gas Turbine Engines.
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This app is made as part of a University Project.
Developed By: Sharaz Ali & Abdulrahman Amer
Supervisor: Dr. Raed Kafafy