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TWO-COMBUSTOR ENGINE FOR MILITARY APPLICATIONS
OPTIMIZATION OF DIRECT OPERATING COSTS OF FUTURE AERO ENGINES
Non-Linear Multiple Point Adaptive Simulation Approach Using Aero-Engine Test-Bed Data
Neural Networks for the Detection of Gas Turbine Sensor Faults
Implications of Subsonic Aero Engine Design and Flight Operations on Atmospheric Pollution
Implications of Low Emissions Requirements on Aircraft Engine Design and Flight Operations
GAS TURBINE FUEL ATOMISATION DYNAMICS UNDER SUB-ATMOSPHERIC CONDITIONS
Gas Turbine Engine and Sensor Diagnostics
FUZZY-LOGIC-BASED DIAGNOSTIC PROCESS FOR TURBOFAN ENGINES