Dersin Bilgileri

Dersin Adı	Türkçe	Sıkıştırılabilir Aerodinamik
	İngilizce	Compressible Aerodynamics
Dersin Kodu	UZB 362E	Kredi	Ders (saat/hafta)	Uygulama (saat/hafta)	Labratuvar (saat/hafta)
Dönem	6	4	4	-	-
Dersin Dili		İngilizce
Dersin Koordinatörü		Hayri Acar
Dersin Amaçları		• To define compressible flow and its effects on governing equations. • To teach shocks and expansion waves and related calculation methods. • To teach linearization of basic equations and validity conditions. • To enable students to calculate the flow field and forces by using the given knowledge.
Dersin Tanımı		Two dimensional subsonic compressible steady and isentropic flows. Linear theory for subsonic and supersonic flows. Supersonic airfoils. Normal shocks. Oblique shocks. Expansion waves. Nozzles, diffusers and wind tunnels.
Dersin Çıktıları		• To define compressible flow and its effects on governing equations. • To teach shocks and expansion waves and related calculation methods. • To teach linearization of basic equations and validity conditions. • To enable students to calculate the flow field and forces by using the given knowledge.
Önkoşullar		AKM 205 or AKM205E
Gereken Olanaklar
Diğer
Ders Kitabı		Fundamentals of Aerodynamics, J.D. Anderson, McGraw-Hill, 2001.
Diğer Referanslar		Aerodynamics for Engineering Students, E.L. Houghton and P.W. Carpenter, Butterworth-Heinemann, 2003. Aerodynamics for Engineers, J.J. Bertin and M.L. Smith, Prentice-Hall, 2008. Modern Compressible Flow: With Historical Perspective, J.D. Anderson, McGraw-Hill, 2002.

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