Course Information

Course Name	Turkish	Sıkıştırılabilir Aerodinamik
	English	Compressible Aerodynamics
Course Code	UZB 310E	Credit	Lecture (hour/week)	Recitation (hour/week)	Laboratory (hour/week)
Semester	2	3	-	-	-
Course Language		English
Course Coordinator		Aydın Mısırlıoğlu
Course Objectives		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.
Course Description		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.
Course Outcomes		On completing this course students should be able to: -Apply basic thermodynamic relations to flow problems. -Analyze normal and oblique shocks and expansion waves calculate flow properties around them. -Calculate compressible internal flows. -Calculate subsonic and supersonic compressible flow properties around airfoils. -Solve basic hypersonic flow problems
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