ASE342 AERODYNAMICS II
| Course Code: | 3840342 |
| METU Credit (Theoretical-Laboratory hours/week): | 4 (3.00 - 2.00) |
| ECTS Credit: | 5.5 |
| Department: | Aerospace Engineering |
| Language of Instruction: | English |
| Level of Study: | Undergraduate |
| Course Coordinator: | Assist.Prof.Dr BARIŞ GÜNGÖRDÜ |
| Offered Semester: | Spring Semesters. |
Course Objectives
Apply the fundamental principles of aerodynamics to predict forces, moments, and heating rates on aircraft through a broad range of speeds and altitudes.?
Course Content
Compressible flow, normal and oblique shock waves, Prandtl-Mayer expansion wave. Subsonic Compressible Flow over Airfoils; Linear Theory, Linearized Supersonic Flow. 2D Boundary layers, concept and governing equations, similar flows and similarity transformation, Blassius problem. Integral methods of solution. Laminar and turbulent flows, stability and transition. Turbulence and transition. Turbulent boundary layers, Law of the wall and various turbulence models, Prandtl mixing length concept. Combined B/L along a flat plate, separation and stall, B/L on airfoils.
Course Learning Outcomes
Program Outcomes Matrix
| Level of Contribution | |||||
| # | Program Outcomes | 0 | 1 | 2 | 3 |
| 1 | ability to apply basic knowledge in mathematics, science, and engineering in solving aerospace engineering problems | ✔ | |||
| 2 | ability to analyze and design aerospace systems and subsystems | ✔ | |||
| 3 | ability to reach knowledge required to solve given problems and utilize that knowledge in solving them | ✔ | |||
| 4 | ability to follow advancements in their fields and improve themselves professionally | ✔ | |||
| 5 | ability to communicate and participate effectively in multi-disciplinary teams | ✔ | |||
0: No Contribution 1: Little Contribution 2: Partial Contribution 3: Full Contribution