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| Section 10: Potential Flow, Lift, and Drag | ||||||||||||
| 10.1 | The occurence of irrotational (potential) flows. The definition of the velocity potential f. | |||||||||||
| 10.2 | Incompressible potential flows as solutions of Laplace's equation for the velocity potential with ∂f/∂n specified at the boundaries (the "Neumann problem"). | |||||||||||
| 10.3 | The equation for the pressure distribution (Bernoulli's integral in terms of f. | |||||||||||
| 10.4 | An example: The solution for 2D potential flow over a cylinder. Comparision with experimental data at high Reynolds number, where the flow might be expected to be reasonably "inviscid." Discussion of the pitfalls of potential flow theory. | |||||||||||
| 10.5 | [Two-dimensional potential flows. Analytic solutions for simple 2D flows: parallel uniform flow, line source or sink, line vortex. Superposition of simple elemental flows as representations of flows over 2D bodies.] | |||||||||||
| 10.6 | Three properties of ideal potential flows around 2D bodies in an infinite stream: (a) The nonexistence of drag (D'Alembert's paradox), (b) the relation between lift and circulation around the body (Kutta-Joukowsky theorem), and (c) the indeterminacy of the circulation in 2D potential flow theory. | |||||||||||
| 10.7 | The Kutta condition: an ad hoc criterion, derived from experimental observation, that allows potential flow analysis to be used to establish the circulation (i.e. lift) for a 2D shape with a sharp trailing edge. | |||||||||||
| 10.8 | Comments on the fact that viscosity, no matter how "small" it may be in a high Reynolds number flow, is responsible by casing separation for the existence of both lift and drag. | |||||||||||
| 10.9 | Qualitative picture of the 3D flow field over a finite lifting surface (wing). Wing-tip vorticies, downwash, etc. Induced drag. | |||||||||||
| 10.10 | Overview of lift and drag forces on lifting surfaces. | |||||||||||
| Reading | ||||||||||||
| Fay, Chapter 11, or, for example, Potter & Foss, pp 360-390, 454-468 | ||||||||||||