Cancellation of crossflow instabilities through multiple discrete roughness elements forcing

Journal Article (2022)
Author(s)

G. Zoppini (TU Delft - Aerodynamics)

Theo Michelis (TU Delft - Aerodynamics)

D. Ragni (TU Delft - Wind Energy)

Kotsonis Marios (TU Delft - Aerodynamics)

Research Group
Aerodynamics
Copyright
© 2022 G. Zoppini, Theodorus Michelis, D. Ragni, M. Kotsonis
DOI related publication
https://doi.org/10.1103/PhysRevFluids.7.123902
More Info
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Publication Year
2022
Language
English
Copyright
© 2022 G. Zoppini, Theodorus Michelis, D. Ragni, M. Kotsonis
Related content
Research Group
Aerodynamics
Issue number
12
Volume number
7
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Abstract

The presented work introduces a cancellation technique, based on the linear superposition of stationary crossflow instabilities (CFIs) through the application of a streamwise series of optimally positioned discrete roughness element (DRE) arrays on a swept wing surface. The DRE arrays are designed and arranged with suitable amplitude and phase shift to induce velocity disturbance systems that destructively interact, ultimately damping the developing CFIs. The robustness of this technique is investigated for a smooth wing surface as well as in the presence of enhanced distributed surface roughness. The resulting flow fields are measured with infrared thermography and particle tracking velocimetry, allowing for the extraction of the laminar-to-turbulent transition front location and for the characterization of the local boundary layer development. The acquired data show that the superposition of suitably arranged DRE arrays can successfully suppress monochromatic CFIs, reducing their amplitude and growth and delaying the boundary layer transition to turbulence when applied on a smooth wing surface. However, the presence of elevated background roughness significantly reduces the effectiveness of the proposed method.