File:Pressure distribution along the circular wall of a wall jet.jpg
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English: Inviscid flow of a wall jet of width h along a circular wall of radius r is calculated using formulae (27) and (29) from L.C. Woods: Compressible subsonic flow in two-dimensional channels with mixed boundary conditions, in: Quart. Journ.Mech.and Applied Math., Vol VII, Pt.3 (1954). The deviation angle must be given for the calculation: the angle found in experiments made by the author M. Kadosch in 1956 was chosen, and is here compared with the separation angle found in a calculation of the separation of the boundary layer due to the calculated pressure gradient along the wall (Kadosch M.: The curved wall effect in: 2nd Cranfield Fluidics Conference, Cambridge, 1967-01-03). Also this theoretical pressure is compared with the experimental pressure along the wall found by the author Kadosch M.: Déviation d'un jet par adhérence à une paroi convexe, in: Journal de Physique et le Radium, Paris, Avril 1958, p. 9A
According to : Van Dyke, M. (1969), Higher-Order Boundary-Layer Theory, Annual Review of Fluid Mechanics, quoted in : "Lift (force)-Wikipedia, the free encyclopedia," the derivation of his equation (4c) shows that the contribution of viscous stress to flow turning is negligible. |
| Date | |
| Source | Own work |
| Author | Marcel kadosch |
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 21:48, 21 February 2016 | | 1,000 × 1,000 (190 KB) | Marcel kadosch | User created page with UploadWizard |
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