Experimental investigation of turbulent separated-reattachment flow by using LDV
Abstract
A turbulent separation-reattachment flow in a two-dimensional asymmetrical curved-wall diffuser was surveyed with a two-dimensional laser doppler velocimeter. The turbulent boundary layer was separated on the lower curved wall under strong pressure gradient and then reattached subsequently on a parallel channel. At the inlet of the diffuser, the Reynolds number based on the diffuser height is 1.2 x 10(exp 5) and the velocity is 25.2 m/s. The results of the experiments in newly defined streamline-aligned coordinates are presented and analyzed. The experiment showed that after Transitory Detachment there was a second extremum of normal Reynolds stress and shear stress appeared as a minus in the near-wall backflow region. A scale was formed using the maximum Reynolds shear stress. It was found that Reynolds shear stress similarity exists from separation to reattachment and the Schofield-Perry velocity law exists in the forward shear flow. Both profiles were used in the experimental work that led to the design of a new eddy-viscosity model. The length scale came from that developed by Schofield and Perry. the composite velocity scale was formed by the maximum Reynolds shear stress and Schofield-Perry velocity scale as well as the edge velocity of the boundary layer. The results of these experiments are presented in this paper.
- Publication:
-
Joint Proceedings on Aeronautics and Astronautics (JPAA)
- Pub Date:
- May 1993
- Bibcode:
- 1993jpaa.proc...23Y
- Keywords:
-
- Coordinates;
- Eddy Viscosity;
- Laser Doppler Velocimeters;
- Pressure Gradients;
- Separated Flow;
- Shear Stress;
- Turbulent Boundary Layer;
- Turbulent Flow;
- Asymmetry;
- Boundary Layer Flow;
- Extremum Values;
- Reynolds Number;
- Shear Flow;
- Wall Pressure;
- Fluid Mechanics and Heat Transfer