Investigation of a three-dimensional turbulent boundary layer with separation in incompressible flow
Abstract
Development of a turbulent boundary layer was studied on the floor of an asymmetric diffuser producing lateral pressure gradients, and longitudinal pressure gradients large enough to cause separation. Maximum flow velocity was 29 m per sec with momentum thickness Reynolds number of 20,000 at separation. Pressure distributions, velocity profiles, viscous layer parameters and flow deflections are discussed. A separation front is defined and the flow beyond it is described. The separation occurs further downstream than it does for a two dimensional case with similar streamwise gradients. The results were examined in relation to Colesa Wake hypothesis and a degree of distortion found to be present.
- Publication:
-
B.S. Thesis Bristol Univ. (England). Dept. of Aeronautical Engineering
- Pub Date:
- June 1980
- Bibcode:
- 1980bue..rept.....A
- Keywords:
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- Separated Flow;
- Three Dimensional Flow;
- Turbulent Boundary Layer;
- Wind Tunnel Tests;
- Flow Visualization;
- Mathematical Models;
- Pressure Distribution;
- Vaneless Diffusers;
- Velocity Distribution;
- Fluid Mechanics and Heat Transfer