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Spatio-temporal statistics of a turbulent boundary layer under unsteady adverse pressure gradients : data from Time-Resolved Particle Image Velocimetry

ORAL

Abstract

An unsteady adverse pressure gradient turbulent boundary layer was created by rapidly deforming a 0.45 m long ceiling panel of a boundary layer wind tunnel to the shape of a convex bump. The spatial strength of pressure gradient and the rate of change of pressure gradient imposed were independently varied using an electropneumatic control mechanism for the ceiling panel. Time-Resolved Particle Image Velocimetry (TR-PIV) was used to capture the response of the boundary layer for a range of adverse pressure gradients. This talk will focus on the spatial and temporal evolution of single- and multi-point turbulent statistics obtained from phase-locked ensemble averages of the TR-PIV data for 3 rates of imposition of pressure gradients corresponding to non-dimensional times, t* (defined as the ratio of convective time scale to imposed unsteady time scale), of 4.38, 1.53, and 0.61. The friction Reynolds number of the incoming flow, Reτ, was 940 and the boundary layer thickness, δ, was 42 mm.

Presenters

  • Aadhy S Parthasarathy

    University of Illinois at Urbana-Champai

Authors

  • Aadhy S Parthasarathy

    University of Illinois at Urbana-Champai

  • Theresa Saxton-Fox

    Department of Aerospace Engineering, University of Illinois Urbana-Champaign, University of Illinois at Urbana-Champaign