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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
Pre-requisite(s)
Required Facilities
Other
Textbook
Other References
 
 
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