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UZB 310E
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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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