Aerodynamics
Aerodynamics support covering aerodynamic loads, potential flow, airfoil theory, panel methods, finite wings, and 3D incompressible flow.
Course Content
Weekly contentAerodynamic forces, moments, dimensionless coefficients, reference area, and core definitions.
Continuity, momentum, and energy approaches; compressible/incompressible, viscous/inviscid, and steady/unsteady flow classifications.
Pressure, pressure forces, and physical interpretation of surface pressure distributions.
Velocity potential, stream function, source, vortex, doublet, and superposition approaches.
Simple potential-flow elements, constructing flow fields, and physical interpretation.
Airfoil geometry, chord, camber, angle of attack, lift, drag, and moment concepts.
Thin airfoil theory, lift-curve slope, zero-lift angle, and moment coefficient.
Pressure distribution on an airfoil, Cp plots, and the lift relationship.
Panel-method logic, discretization, boundary conditions, and physical evaluation of results.
Aspect ratio, induced drag, downwash, and the Prandtl lifting-line approach.
Three-dimensional wing effects, spanwise flow, wingtip vortices, and basic interpretation.
Past exam questions, homework problems, modeling strategies, and solution practice.
Targeted Learning Outcomes
- Interpret aerodynamic force and moment concepts physically
- Solve problems with potential flow and thin airfoil theory
- Understand panel-method logic and evaluate results
- Use finite wing theory to calculate induced drag and downwash
Recommended Prerequisites
- Fluid mechanics with the control-volume approach
- Calculus and basic linear algebra are useful
- Thermodynamics is useful for compressibility topics