Course Information

Course Name	Turkish	Dönerkanatlı Havaaracı Yapısal Dinamiği ve Aeroelastisitesi
	English	Rotorkraft Yapısal Dinamiği ve Aeroelastisite (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		Ali Tatar
Course Objectives		- To introduce the fundamentals of rotorcraft structural dynamics and aeroelasticity - To show practical engineering applications and recent research activities in the field.
Course Description		1) Introduction 2) Structural Dynamics Review 3) Dynamics of Rotor Models 4) Rotorcraft Vibrations 5) Vibration Control Methods in Rotorcraft 6) Mechanical and Aeromechanical Instabilities 7) Vibration Testing and Experimental Modal Analysis 8) Further Research Topics
Course Outcomes
Pre-requisite(s)		Fundamental maths and physics, mechanical vibrations
Required Facilities
Other
Textbook		Rotary Wing Structural Dynamics and Aeroelasticity Richard L. Bielawa AIAA Education Series Second Edition, 2006
Other References		1) Johnson, Wayne: Rotorcraft Aeromechanics, Cambridge University Press, Boston, Massachusetts, 2012. 2) Friswell, Michael I., John E. T. Penny, Seamus D. Garvey, and Arthur W. Lees.: Dynamics of Rotating Machines, Cambridge University Press, 2010. 3) Inman, Daniel J.: Engineering Vibration, 4th Edition, Pearson.