Program Gas Turbine :

• Complete Turbo-Jet / Turbo-Fan Engines Cycle Analysis.

• Complete Engine Performance Analysis.

• Rate of Change Of All Outputs With Respect to Time / Flight Parameters / Engine Specifications / Engine Inputs.

• All Engines May Equipped With An After-Burner.

• Turbo-Fan Engines May Have Mixed / Seperate Out-Flow.

Special Tools :

• Engine Design For Optimization.

• Super-Sonic Axial Flow Compressor Design.

• Combustion Chamber Design Tool By Eng.Ahmed Omran.

• Supersonic Nozzle Design Tool By Eng.O.S.