The Effect of Free-Stream Forcing on a Turbulent Boundary Layer

POSTER

Abstract

This work investigated the interactions within a zero-pressure gradient turbulent boundary layer in the presence of free-stream external forcing. Controlled generation of energetic large-scale coherent structures was achieved by oscillating a NACA-0010 airfoil section of 8-inch chord length positioned at the entrance to a wind tunnel at mid-section height. This resulted in carefully controlled large-scale structures being introduced by free-stream perturbations. The amplitude and frequency of oscillation were independently varied, and the interactions within the resultant boundary layer were measured by means of a traversing hot-wire probe positioned about 3.0 m downstream of the trailing edge. Measurements were carried out at two friction Reynold’s numbers (Reτ) of approximately 1770 and 2500, respectively. The free-stream forcing was observed to have penetrated deep into the boundary layer as the flow developed downstream. The resultant energy spectra showed that this introduced scale reached the near-wall region. Hence, this method for generating controlled large-scale structures was found to be an effective technique to generate controllable, large-scale wall shear stress fluctuations.

*This research was sponsored by the Army Research Office and was accomplished under Grant Number W911NF-22-1-0253. The views and conclusions contained in this document are those of the authors and should not be interpreted as representing the official policies, either expressed or implied, of the Army Research Office or the U.S. Government. ​

Presenters

  • Robert H Bryan

    • Embry-Riddle Aeronautical University

Authors

  • Robert H Bryan

    • Embry-Riddle Aeronautical University
  • Vaishak Thiruvenkitam

    • Embry-Riddle Aeronautical University
  • Zheng Zhang

    • Embry-Riddle Aeronautical University-Worldwide
  • Ebenezer P Gnanamanickam

    • Embry-Riddle Aeronautical University-Worldwide