AEE438 AIRCRAFT ENGINE DESIGN

Course Code:5720438
METU Credit (Theoretical-Laboratory hours/week):3 (2.00 - 2.00)
ECTS Credit:12.0
Department:Aerospace Engineering
Language of Instruction:English
Level of Study:Undergraduate
Course Coordinator:Assoc.Prof.Dr. NİLAY SEZER UZOL
Offered Semester:Fall Semesters.

Course Objectives


Course Content

Calculation of required and available specific thrust and impulse at various flight phase of the mission for a turbojet, turbofan and turboprop engine. Calculation of performance characteristics of aircraft engine components such as inlet, fan, compressor, combustor, turbine, afterburner and nozzle. Component matching and calculations of total temperature and pressure ratios of each component at different rotational speeds and mass flow rates.


Course Learning Outcomes


Program Outcomes Matrix

Contribution
#Program OutcomesNoYes
1An ability to identify, formulate, and solve complex engineering problems by applying principles of engineering, science, and mathematics
2An ability to apply engineering design to produce solutions that meet specified needs with consideration of public health, safety, and welfare, as well as global, cultural, social, environmental, and economic factors
3An ability to communicate effectively with a range of audiences
4An ability to recognize ethical and professional responsibilities in engineering situations and make informed judgments, which must consider the impact of engineering solutions in global, economic, environmental, and societal contexts
5An ability to function effectively on a team whose members together provide leadership, create a collaborative and inclusive environment, establish goals, plan tasks, and meet objectives
6An ability to develop and conduct appropriate experimentation, analyze and interpret data, and use engineering judgment to draw conclusions
7An ability to acquire and apply new knowledge as needed, using appropriate learning strategies