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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 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 1. Introduction to Aeroelastic Phenomena 2. Static Aeroelasticity: Divergence (Torsion spring model) 3. Control Surface Reversal (TS model) 4. Divergence of a wing via beam model. 5. Structural and aerodynamic influence coefficients 6. Divergence of a wing via matrix model. 7. Matrix model of aileron reversal. 8. Midterm Exam 9. Dynamic Aeroelasticity: Equations of Motion 10. Flutter- Introduction.The nature of flutter. 11. Flutter of a simple system with one degree of freedom 12. Flutter of a simple system with two degrees of freedom 13. Practical flutter analysis tecniques. V-g method 14. Gust Response Dersin Çıktıları Önkoşullar Gereken Olanaklar Diğer Ders Kitabı Diğer Referanslar

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