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Dersin Bilgileri

Dersin Adı
Türkçe Aeroelastisite (Aeroelasticity)
İngilizce (Aeroelasticity
Dersin Kodu
UUM 533 Kredi Ders
(saat/hafta)
Uygulama
(saat/hafta)
Labratuvar
(saat/hafta)
Dönem -
- 3 - -
Dersin Dili Türkçe
Dersin Koordinatörü Metin Orhan Kaya
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 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.
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.
 
 
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