Separation Bubbles Under Steady and Periodic-Unsteady Main Flow Conditions

Author:

Lou Weiliang1,Hourmouziadis Jean1

Affiliation:

1. Jet Propulsion Laboratory, Aerospace Institute F1, Berlin University of Technology, Marchstr. 12, D-10587 Berlin, Germany

Abstract

Based on an experimental investigation carried out in a low-speed test facility at the Berlin University of Technology, this paper describes the formation of separation bubbles under steady and periodic-unsteady main flow conditions. The aim of the investigation was to understand the mechanism of separation, transition, and reattachment, and the effect of main flow unsteadiness on it. Separation bubbles for various main flow conditions were generated over a large flat plate, which experienced a similar pressure distribution to that on the suction surface of blades in turbomachines. The pressure distribution was generated by a contoured wall opposite the plate. Aimed at separating the effect of the velocity and the turbulence wake, this paper considers only the influence of the velocity wake. To this effect, a rotating flap was mounted downstream of the test section to produce periodic oscillations of the main flow. The overall flow field under steady main flow conditions was obtained by hot-wire measurements. Pressure taps were used to measure the pressure distribution over the plate. The Reynolds number effects were determined and compared to the measurement results in the literature. Results for periodic-unsteady separation bubbles are shown using different Strouhal numbers, oscillation amplitudes, and Reynolds numbers. Ensemble-averaged mean velocity profiles and the ensemble-averaged rms velocity profiles are used to demonstrate the development of the periodic boundary layer. Time–space diagrams are plotted to show the development of the periodic-unsteady boundary layers. The characteristic instability frequencies in the free shear layer are identified. The impact of the major parameters, Strouhal number and amplitude, on the bubble formation are discussed. [S0889-504X(00)01204-6]

Publisher

ASME International

Subject

Mechanical Engineering

Reference23 articles.

1. Hodson, H. P., 1991, “Aspect of Unsteady Blade-Surface Boundary Layers and Transition in Axial Turbomachines,” VKI Lecture Series 1991-06, Boundary Layers in Turbomachines, Sept. 2–6.

2. Hourmouziadis, J., 1989, “Aerodynamic Design of Low Pressure Turbines,” AGARD Lecture Series 167.

3. Walker, G. J. , 1993, “The Role of Laminar–Turbulent Transition in Gas Turbine Engines: A Discussion,” ASME J. Turbomach., 115, pp. 207–217.

4. Mayle, R. E. , 1991, “The Role of Laminar–Turbulent Transition in Gas Turbine Engines,” ASME J. Turbomach., 113, pp. 509–537.

5. Gault, D. E., 1955, “An Experimental Investigation of Regions of Separated Laminar Flow,” NACA TN 3505.

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