Higher approximations in boundary-layer theory Part 1. General analysis
- 1 September 1962
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of Fluid Mechanics
- Vol. 14 (2) , 161-177
- https://doi.org/10.1017/s0022112062001147
Abstract
Prandtl's boundary-layer theory is embedded as the first step in a systematic scheme of successive approximations for finding an asymptotic solution for viscous flow at large Reynolds number. The technique of inner and outer expansions is used to treat this singular-perturbation problem. Only analytic semi-infinite bodies free of separation are considered. The second approximation is analysed in detail for steady laminar flow past plane or axisymmetric solid bodies. Attention is restricted to low speeds and small temperature changes, so that the velocity field is that for an incompressible fluid, the temperature field being calculated subsequently. The additive effects are distinguished of longitudinal curvature, transverse curvature, external vorticity, external stagnation enthalpy gradient, and displacement speed. The effect of changing co-ordinates is examined, and the behaviour of the boundary-layer solution far downstream discussed. Application to specific problems will be made in subsequent papers.Keywords
This publication has 8 references indexed in Scilit:
- Boundary Layer Over a Flat Plate in Presence of Shear FlowPhysics of Fluids, 1960
- Vorticity Effect on the Stagnation-Point Flow of a Viscous Incompressible FluidJournal of the Aerospace Sciences, 1959
- On Asymptotic Expansions in the Theory of Boundary LayersJournal of Mathematics and Physics, 1957
- On Laminar Boundary Layers With Heat TransferJournal of Jet Propulsion, 1956
- The role of coordinate systems in boundary-layer theoryZeitschrift für angewandte Mathematik und Physik, 1954
- Readers ForumJournal of the Aeronautical Sciences, 1954
- Some Effects of Surface Curvature on Laminar Boundary-Layer FlowJournal of the Aeronautical Sciences, 1953
- Skin-Friction and Heat-Transfer Characteristics of a Laminar Boundary Layer on a Cylinder in Axial Incompressible FlowJournal of the Aeronautical Sciences, 1951