Incompressible Flow II
£5.25
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Incompressible Flow II
£5.25
Part 2 of 2 in the Incompressible Flow series. Topics in this product include the Kutta-Joukowski theorem, conformal transformation, pressure distribution on flat-plate and cambered aerofoils, panel methods, and lifting-line theory through to Prandtl's equation and the elliptic lift distribution.
This is a 17-page PDF scan of handwritten notes, featuring clickable PDF bookmarks so you can jump straight to any page in a PDF viewer such as Adobe Acrobat. Complete page-by-page contents can be found below so you know exactly what's inside before you buy.
AerodynamicsPage-by-page contents
Aerodynamics
Page-by-page contents
- 01Relationship between lift and circulation, Kutta-Joukowski theorem
- 02Flow around circular cylinder, generating circulation in a cylinder
- 03Rigid boundaries, method of images, basic solutions for complex potential
- 04Conformal transformation, example
- 05Flow past ellipse at zero incidence, flow past ellipse at incidence
- 06Kutta-Joukowski condition, drag in a real airfoil, starting vortex
- 07Pressure distribution on a flat plate airfoil using Joukowski transformation
- 08Cambered flat plate and thick airfoil by Joukowski transformation
- 09Effects of thickness and camber, superposition of solutions
- 10Surface singularity methods, source distribution, vorticity distributions
- 11Lumped vortex model, panel code
- 12Lifting line theory
- 13Downwash and circulation, Prandtl lifting line equation
- 14Prandtl theory for large AR wings derivation
- 15Applying lifting line theory, generalised lift distribution lifting line solution
- 16Total lift, total induced drag, elliptic distribution
- 17Solution for general planforms: collocation method