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GAZ TÜRBİNLİ MOTORLAR VE UYGULAMALARI I COURSE IDENTIFICATION AND APPLICATION INFORMATION

Code Name of the Course Unit Semester In-Class Hours (T+P) Credit ECTS Credit
GMY353 GAZ TÜRBİNLİ MOTORLAR VE UYGULAMALARI I 5 8 7 5

KEY LEARNING OUTCOMES OF THE COURSE UNIT (On successful completion of this course unit, students/learners will or will be able to)

Explains the basic operating principles of gas turbine engines; evaluates the relationship between potential energy, kinetic energy, Newton’s laws of motion, and the Brayton cycle.
Analyzes the relationship between engine power, force, work, energy, speed, and acceleration; determines their impact on the design and performance of gas turbine engines.
Compares the structural characteristics of turbojet, turbofan, turboshaft, and turboprop engines; examines the operating principles of each engine type and analyzes their differences in industrial applications.
Defines the performance parameters of gas turbine engines; evaluates the impact of key metrics such as gross thrust, net thrust, converging nozzle thrust, thrust distribution, and specific fuel consumption (SFC) on engine performance.
Assesses how environmental factors affect engine performance; determines the influence of parameters such as bypass ratio, engine pressure ratio, and gas flow temperature, pressure, and velocity on engine performance.
Explains engine ratings and performance limitations; investigates the effects of static thrust, speed-altitude-temperature relationships on engine performance.
Analyzes the structure and operation of compressor inlet systems; evaluates the impact of different inlet configurations on engine performance and discusses ice protection methods.
Examines the structure, operating principles, and applications of compressors; distinguishes between axial and centrifugal types, and analyzes the effects of fan balancing methods on engine performance.
Explains the occurrence of stall and surge in compressors; analyzes their causes and effects on engine performance. Evaluates the effectiveness of airflow control methods such as bleed valves, variable inlet guide vanes, variable stator vanes, and rotating stator blades.
Explains the structural characteristics and operating principles of the combustion section; determines the impact of combustion chamber design on the efficiency of gas turbine engines.