Application of Acoustic Metamaterials in Boundary Layer Instability Control

Master Thesis (2021)
Author(s)

C.L.A. de Koning (TU Delft - Aerospace Engineering)

Contributor(s)

M Kotsonis – Mentor (TU Delft - Aerodynamics)

Theodorus Michelis – Mentor (TU Delft - Aerodynamics)

Faculty
Aerospace Engineering
Copyright
© 2021 Coert de Koning
More Info
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Publication Year
2021
Language
English
Copyright
© 2021 Coert de Koning
Graduation Date
23-04-2021
Awarding Institution
Delft University of Technology
Programme
Aerospace Engineering | Aerodynamics and Wind Energy
Faculty
Aerospace Engineering
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Abstract

To achieve delay of laminar-to-turbulent transition of boundary layers, the application of acoustic metamaterial concepts is investigated. This is done analytically, numerically and experimentally by studying the interaction between a Helmholtz resonator and a TS wave. A Helmholtz resonator can serve as a meta-atom in a metamaterial. The desired wall controller property of a metamaterial to suppress TS waves is evaluated. This study shows that TS wave attenuation is achieved if the wall-normal velocity from a metamaterial is in-phase with the TS wave pressure. TS wave amplification is obtained if the pressure and velocity are more than (approximately) 90 degrees out of phase. The p-v phase relation corresponding to a Helmholtz resonator only remains in the amplification regime. Therefore, the conclusion is drawn that a single Helmholtz resonator can only amplify TS waves. If an acoustic metamaterial concept is found where pressure and wall-normal velocity are in-phase, this can be useful in boundary layer instability control.

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