Dersin Bilgileri

Dersin Adı	Türkçe	Aeroelastisite
	İngilizce	Aeroelasticity
Dersin Kodu	UCK 472E	Kredi	Ders (saat/hafta)	Uygulama (saat/hafta)	Labratuvar (saat/hafta)
Dönem	7	3	3	-	-
Dersin Dili		İngilizce
Dersin Koordinatörü		Metin Orhan Kaya
Dersin Amaçları		Understand the effects of various aeroelastic properties on the design and performance of aeronautical vehicles. Students should be able to quantify the effects of the inertial, structural and aerodynamic parameters that affect divergence, control surface reversal and flutter. Students should be able to calculate critical speeds for these phenomena for simple wings using steady, and in the case of flutter, quasi-steady aerodynamic assumptions.
Dersin Tanımı		Introduction to aeroelasticity: Definition, historical background. Static Aeroelastic Phenomena: Divergence, aileron effectiveness and reversal, twisting of simple two-dimensional wing with aileron. Flutter: The nature of flutter, flutter of simple system with one and two degrees of freedom, V-g method.
Dersin Çıktıları
Önkoşullar
Gereken Olanaklar
Diğer
Ders Kitabı		Raymond L. Bishlinghoff, Holt Ashley ve Robert L. Halfman, Aeroelasticity, Dover Edition, 1996
Diğer Referanslar		Dowell, E. H., Crawley, E. F., Curtiss Jr., H. C., Peters, D. A., Scanlan, R. H., and Sisto, F., A Modern Course in Aeroelasticity, Kluwer Academic Publishers, 3rd Edition, 1995.