Eskisehir Technical University Info Package Eskisehir Technical University Info Package
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About the Program Educational Objectives Key Learning Outcomes Course Structure Diagram with Credits Field Qualifications Matrix of Course& Program Qualifications Matrix of Program Outcomes&Field Qualifications
  • Institute of Graduate Programmes
  • Department of Avionics
  • Master of Science (MS) Degree
  • Course Structure Diagram with Credits
  • Parametric Cycle Analysis of Aircraft Propulsion System
  • Learning Outcomes & Program Qualifications
  • Description
  • Learning Outcomes
  • Course's Contribution to Prog.
  • Learning Outcomes & Program Qualifications
  • ECTS Credit Load
0 : Does not support   1 : Low-level support   2 : Mid-level support   3 : Top level support
Learning Outcomes12345678910
Analysing of aircraft propulsion parametric cycles through numerical methods. ----------
structural arrangements and studies of turbojet, turbofan, turboshaft, turboprop engines----------
Engine Performance Gross thrust, net thrust, conical nozzle thrust, thrust distribution, resulting thrust, thrust horsepower, equivalent shaft horsepower, specific fuel consumption----------
Engine efficiencies; Bypass ratio and engine pressure ratio----------
Pressure, temperature and speed of gas flow; Engine types, static thrust, effects of speed-altitude-hot climate, flat rating limitations----------
Compressor inlet data; Effect of different input configurations; Protection from ice.;Compressors Axial and centrifugal types; Structural features, operating principles and applications----------
Fan balancing; His work; Causes and effects of compressor stalling and surge; Airflow control methods: bleed valves, variable inlet guide vanes, variable stator vanes, rotating stator blades; Compressor compression ratio----------
Combustion Part Structural features and operating principles. Turbine Part Operation and characteristics of various turbine blade types; Connecting the pallet to the disk; Nozzle guide vanes; Causes and effects of turbine blade stress and temperature.----------
Exhaust Structural properties and operating principles; Collector, distributor and variable area nozzles; Reducing engine noise; Reaction direction reversors.; Bearings and Gaskets. Structural features and operating principles. Lubricants and Fuels Features and specifications; Fuel additives; Security measures.----------
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