Boundary Layers III
£5.25
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Boundary Layers III
£5.25
Part 3 of 4 in the Boundary Layers series. Topics in this product include compressible boundary layers, similarity and viscous parameters, Reynolds' analogy and the reference temperature method, viscous interaction, entropy layers, and hypersonic boundary layer transition.
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
- 01Compressible boundary layers, boundary layer equations, similarity vs viscous parameters
- 02Momentum equations, thin boundary layers at high Re, temperature gradients in low speed flow
- 03Temperature gradients in high speed flow
- 04Temperature profiles in boundary layers, hot and cold wall cases, temperature gradient
- 05Reynolds' analogy, Reynolds' number, Prandtl number, steady laminar boundary layer on flat plate
- 06Scaling compressible boundary layers, similarity solutions for flat plate, effect of Mach number
- 07Effect of compressibility on skin friction and Stanton number, hot vs cold walls
- 08Reference temperature, T*, examples with turbulent and laminar cases
- 09Reference parameters in turbulent and laminar cases, example (continued)
- 10Compressible flow around a stagnation point, Van Driest equation
- 11Viscous interaction, strong vs weak interaction
- 12Viscous similarity parameter, strong vs weak viscous interaction
- 13Example
- 14Entropy layers
- 15Entropy layer swallowing
- 16Hypersonic boundary layer transition, Reynolds transition number, effect of Mach number and wall temperature
- 17Effect of nose radius, pressure gradient, and surface roughness on boundary layer