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PROPULSION SYSTEMS COURSE IDENTIFICATION AND APPLICATION INFORMATION

Code Name of the Course Unit Semester In-Class Hours (T+P) Credit ECTS Credit
UCK306E PROPULSION SYSTEMS 6 3 3 4

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

Recognizing aircraft engines and understanding classification basis
Understanding how thrust established by aircraft engines
Understanding primary performance parameters in aircraft engines
Understanding how to use thermodynamic cycles on performance analysis at aircraft engines
Understanding the effects of reaction heat, adiabatic flame temperature on overall performance about combustion chambers of aircraft engines.
Ability to calculate the ideal performances at design conditions of aircraft engines and their components
Understanding the inclusion of losses and their effects due to the components of aircraft engines on the overall performance analysis.
Ability to calculate the aircraft performance values and evaluate them at realistic cases whit losses.
Ability to carry out aircraft engine performance analysis and interpretation.