Course Information

Course Name	Turkish	Sıkıştırılabilir Aerodinamik
	English	Compressible Aerodynamics
Course Code	UZB 362E	Credit	Lecture (hour/week)	Recitation (hour/week)	Laboratory (hour/week)
Semester	6	4	4	-	-
Course Language		English
Course Coordinator		Hayri Acar
Course Objectives		• 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.
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		• 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.
Pre-requisite(s)		AKM 205 or AKM205E
Required Facilities
Other
Textbook		Fundamentals of Aerodynamics, J.D. Anderson, McGraw-Hill, 2001.
Other References		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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