On the Three-Dimensional Structure of Turbulent Spots

Author:

Chong T. P.1,Zhong S.1

Affiliation:

1. School of Engineering, University of Manchester, Manchester M13 9PL, UK

Abstract

A detailed measurement of turbulent spots propagating in a laminar boundary layer over a flat plate was made at a zero pressure gradient and three favorable pressure gradients. Data were recorded across the span of turbulent spots at a number of streamwise locations along the plate using a hot-wire probe and surface-mounted hot films. In this work we aim at extending the existing studies that are largely based upon measurements made in the plane of symmetry of the spots and away from the wall and investigating the three-dimensional structure of turbulent spots and its dependence on streamwise pressure gradients. The results from the present experiment reveal some interesting aspects of the overall structure of the spots and the role that regions with negative velocity perturbations play in the spanwise growth of turbulent spots. The presence of a spanwise overhang is also confirmed that is believed to be responsible for the smaller spreading angle of spots measured at the wall. This finding is expected to have important implications to the development of improved transition models that are used to predict heat transfer and skin friction for turbine blades.

Publisher

ASME International

Subject

Mechanical Engineering

Reference14 articles.

1. Mayle, R. E. , 1991, “The Role of Laminar–Turbulent Transition in Gas Turbine Engines,” ASME Paper No. 91-GT-261.

2. Wygnanski, I. , 1978, “On the Possible Relationship Between the Transition Process and the Large Coherent Structures in Turbulent Boundary Layers,” AFOSR∕Lehigh University Workshop on Coherent Structure of Turbulent Boundary Layers, edited by C. R.Smith and D. E.Abbott, p. 168.

3. The Laminar–Turbulent Transition in a Boundary Layer—Part I;Emmons;J. Aerosp. Sci.

4. Schubauer, G. B., and Klebanoff, P. S., 1955, “Contribution on the Mechanism of Boundary Layer Transition,” NACA TN-3489.

5. Effects of Streamwise Pressure Gradient on Turbulent Spot Development;Gostelow;ASME J. Turbomach.

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