Course Information

Course Name	Turkish	Dönerkanatlı Havaaracı Yapısal Dinamiği ve Aeroelastisitesi
	English	Rotorcraft Structural Dynamics and Aeroelasticity
Course Code	UUM 605E	Credit	Lecture (hour/week)	Recitation (hour/week)	Laboratory (hour/week)
Semester	-	3	3	-	-
Course Language		English
Course Coordinator		Özge Özdemir
Course Objectives		To introduce students to the fundamentals of rotorcraft dynamics and aeroelasticity, and to provide necessary background to equip students to do additional research and analysis in the field.
Course Description		Bu ders kapsamında; helikopter palleri rijit hareket dinamiği, helikopter aerodinamiği ve helikopter aeroelastsitesi konuları detaylı bir biçimde işlenmektedir.
Course Outcomes		After completing this lecture successfully, the students are expected to have knowledge about 1. Helicopter aerodynamics 2. Helicopter blade rigid motion (flapping, lead-lag and pitching) structural dynamics 3. Stability in hover and forward flight conditions 4. Aeroelastic analysis
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Required Facilities
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