AEE728 UNSTEADY AERODYNAMICS
Course Code: | 5720728 |
METU Credit (Theoretical-Laboratory hours/week): | 3 (3.00 - 0.00) |
ECTS Credit: | 8.0 |
Department: | Aerospace Engineering |
Language of Instruction: | English |
Level of Study: | Graduate |
Course Coordinator: | |
Offered Semester: | Fall Semesters. |
Course Objectives
By the end of this course, the student is expected to have acquired knowledge on:
- Fundamental physics governing the unsteady flows;
- Derivation of the unsteady governing conservation equations and simplifications;
- Analytical and numerical analysis of incompressible steady flows;
- Unsteady incompressible flow field and force generation of thin airfoils undergoing a simple harmonic and arbitrary motions;
- Steady and unsteady incompressible flow about thin wings;
- Moderns subjects such as vortex lift and flapping-wing aerodynamics.
Course Content
Overview of steady incompressible and compressible aerodynamics. Unsteady conservation equations. Potential flow and acceleration potential. Steady and unsteady flow about flat plates and thin airfoils. Unsteady Kutta condition. Simple harmonic motion of thin airfoils(Theodorsens theory). Impulsive motion. Returning wake problem (Loewys problem). Arbitrary motion and Wagner function. Gust response and Küssner function. Incompressible unsteady flows about thin wings. Static and dynamic stall. The vortex lift (Polhamus theory). Flapping-wing theory.