Welcome, Guest . Login . Türkçe
Where Am I: Ninova / Courses / Faculty of Aeronautics and Astronautics / UCK 351E / Course Informations
 

Course Information

Course Name
Turkish Aerodinamik
English Aerodynamics
Course Code
UCK 351E Credit Lecture
(hour/week)
Recitation
(hour/week)
Laboratory
(hour/week)
Semester -
4 4 - -
Course Language English
Course Coordinator Melike Nikbay
Course Objectives 1.To give the fundamentals of incompressible aerodynamics 2.To solve basic aerodynamics problems
Course Description Aerostatic. Aerodynamic forces and moments. Fundamental principles and equations. Flow types. Potential flow approach. One dimensional potential flows. Airfoil aerodynamics. Two dimensional potential flows. Thin airfoil theory, 2-D panel methods. Finite wing theory. 3-D incompressible flow
Course Outcomes Student, who passed the course satisfactorily can:
1. Know the basic equations for inviscid incompressible flow
2. Apply conservation of mass and momentum equations to control volume 3. Find the potential and stream functions for the flow around bosies and calculate the pressure distribution
4. Calculate the lift and moment coefficients by using thin airfoil theory
5. Calculate the lift and drag for finite wings at different planforms
Pre-requisite(s)
Required Facilities
Other To get visa for final exam, students need to submit at least 7 homework and the homework average grade should be 40/100
Textbook John D.Anderson, Fundamentals of Aerodynamics, 5th edition, McGraw-Hill
Other References
 
 
Courses . Help . About
Ninova is an ITU Office of Information Technologies Product. © 2024