Metamaterials for Laminar Flow Control on a Wing
MetaWing aims to develop metamaterials to control wave-like instabilities in laminar flows, reducing aircraft drag and emissions by delaying the transition to turbulence.
Projectdetails
Introduction
Achieving extensive laminar flow can reduce aircraft drag by up to 15%, offering breakthrough potential for curbing polluting emissions in aviation and other energy-intensive sectors. To achieve this, wave-like flow instabilities growing in laminar boundary layers need to be controlled and attenuated to delay the transition from laminar to turbulent flow. However, their complex, multi-scale, and broadband nature makes these instabilities extremely challenging to control.
Concept Overview
In MetaWing, I propose a new disruptive concept for flow control, first born in classical wave physics: Metamaterials. These are engineered composite structures that invoke dispersive wave phenomena to gain exotic properties that go beyond what is considered possible in Nature.
Key Property: Bandgap
The main property I want to explore is the bandgap, a range in which waves are suppressed when interacting with the Metamaterial. My team and I have recently found key evidence of dispersive wave suppression in boundary layers. However, wave-like flow instabilities have key differences from classical waves, forming a new regime of dispersive wave interactions. Thus, the nature of bandgaps in boundary layer flows remains unclear and unexplored.
Research Objectives
I aim to reveal and understand the formation of bandgaps in transitional fluid flows and use them to suppress wave-like boundary layer instabilities, thus delaying laminar-turbulent transition.
Methodology
To achieve this, I propose the first holistic intersection of Metamaterials and Laminar Flow Control using:
- Theory
- Numerical simulations
- Novel fabrication methods
- State-of-the-art experimental measurements
Expected Outcomes
The combined results will uncover the complex dynamic behavior of flow instabilities under dispersive interaction with Metamaterials and will help us understand and fully exploit bandgap mechanisms in transitional flows.
Future Impact
MetaWing will create a new class of Metamaterials for flow control and pave the way for ultra-low drag wings for the next generation of emission-free aviation.
Financiële details & Tijdlijn
Financiële details
Subsidiebedrag | € 2.374.014 |
Totale projectbegroting | € 2.374.014 |
Tijdlijn
Startdatum | 1-11-2024 |
Einddatum | 31-10-2029 |
Subsidiejaar | 2024 |
Partners & Locaties
Projectpartners
- TECHNISCHE UNIVERSITEIT DELFTpenvoerder
Land(en)
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This project aims to understand the interaction between acoustic waves and turbulent boundary layers using numerical simulations to improve acoustic characterization and design efficient, low-noise aircraft surfaces.
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This project aims to develop and validate a theory for intermediate-strain turbulence using machine learning and advanced simulations to enhance engineering applications like wind energy and UAV efficiency.
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