The structure of a three-dimensional turbulent boundary layer
- 1 May 1993
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of Fluid Mechanics
- Vol. 250, 43-68
- https://doi.org/10.1017/s0022112093001375
Abstract
The three-dimensional turbulent boundary layer is shown to have a self-consistent two-layer asymptotic structure in the limit of large Reynolds number. In a streamline coordinate system, the streamwise velocity distribution is similar to that in two-dimensional flows, having a defect-function form in the outer layer which is adjusted to zero at the wall through an inner wall layer. An asymptotic expansion accurate to two orders is required for the cross-stream velocity which is shown to exhibit a logarithmic form in the overlap region. The inner wall-layer flow is collateral to leading order but the influence of the pressure gradient, at large but finite Reynolds numbers, is not negligible and can cause substantial skewing of the velocity profile near the wall. Conditions under which the boundary layer achieves self-similarity and the governing set of ordinary differential equations for the outer layer are derived. The calculated solution of these equations is matched asymptotically to an inner wall-layer solution and the composite profiles so formed describe the flow throughout the entire boundary layer. The effects of Reynolds number and cross-stream pressure gradient on the cross-stream velocity profile are discussed and it is shown that the location of the maximum cross-stream velocity is within the overlap region.Keywords
This publication has 4 references indexed in Scilit:
- Application of FEM Modeling to Simulate Metal Flow in Forging a Titanium Alloy Engine DiskJournal of Engineering for Industry, 1983
- The large reynolds number, asymptotic theory of turbulent boundary layersInternational Journal of Engineering Science, 1972
- On Combined Free and Forced Convection in ChannelsJournal of Heat Transfer, 1960
- Turbulent Boundary Layers in Adverse Pressure GradientsJournal of the Aeronautical Sciences, 1954