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
Last updated on Dec 16, 2015
Version 2.0.1:
- Bug Fixes
- User Interface Changes
Version 2.0:
- Design Point Analysis of Turbofan and Turboprop Engines in addition to Turbojet.
- Graph Mode: Allows Plotting of Design Variables versus Performance Parameters.
- Save Results and Graphs.
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