The Delft Laminar Hump: A novel local surface geometry for passive laminarization of aircraft wings
The Delft Laminar Hump project aims to develop a cost-effective, passive wing modification to enhance laminar flow, reducing aircraft drag and emissions, and facilitating industrial adoption.
Projectdetails
Introduction
The exponential growth in aviation calls for radical new technologies to curb aircraft fuel consumption and emissions. At the heart of the problem lies aerodynamic drag. Laminarization, namely the extension of laminar flow over the wing, holds immense potential for reducing aerodynamic drag by up to 15%. Unfortunately, many solutions proposed so far are costly, complex, and unreliable, thus obstructing laminarization from reaching industrial-scale application.
Project Overview
The Delft Laminar Hump aims at breakthrough efficient, robust, and effective laminarization of aircraft wings. The Hump is a fully passive localized geometry modification of the wing surface, discovered by the PI and his team through their research on laminar flow control.
Preliminary Results
In their preliminary experiments, the team has demonstrated a significant laminarization effect and has recently proceeded with an initial patent application.
Objectives
DeLaH aspires to be the first step in transitioning the Hump concept from laboratory to innovation and societal impact. Technical activities are planned towards:
- Validating the concept in wind tunnel tests at conditions resembling cruise flight.
- Documenting the influence of real-life environmental factors such as roughness.
Innovation Activities
Innovation activities cover a diverse range of objectives, such as:
- Strengthening and extending IPR.
- Defining a technology transfer strategy from HI to key industrial stakeholders, such as Airbus.
- Conducting a market and feasibility analysis combined with a business development plan to explore and exploit industrial and research collaborations.
Collaboration
The PI and team will work closely with a group of stakeholders within the HI, such as:
- The Impact and Innovation Centre, providing expertise in IPR and business development.
- The Aerospace Innovation Hub, providing an engaging platform to industrial partners.
Conclusion
Ultimately, the project will strive to position the Hump technology at the starting line of technological development and industrial adoption.
Financiële details & Tijdlijn
Financiële details
Subsidiebedrag | € 150.000 |
Totale projectbegroting | € 150.000 |
Tijdlijn
Startdatum | 1-1-2024 |
Einddatum | 30-6-2025 |
Subsidiejaar | 2024 |
Partners & Locaties
Projectpartners
- TECHNISCHE UNIVERSITEIT DELFTpenvoerder
Land(en)
Vergelijkbare projecten binnen European Research Council
Project | Regeling | Bedrag | Jaar | Actie |
---|---|---|---|---|
Metamaterials for Laminar Flow Control on a WingMetaWing aims to develop metamaterials to control wave-like instabilities in laminar flows, reducing aircraft drag and emissions by delaying the transition to turbulence. | ERC Consolid... | € 2.374.014 | 2024 | Details |
Discovering novel control strategies for turbulent wings through deep reinforcement learningDEEPCONTROL aims to enhance aviation sustainability by using deep reinforcement learning and high-fidelity simulations for real-time flow control around wings, reducing fuel consumption and emissions. | ERC Consolid... | € 1.999.748 | 2022 | Details |
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MOdeling and Reduction of Aeroacoustics Sources of Interaction Noise in AviationThe project aims to develop a holistic acoustic model for predicting interaction noise in aviation by understanding flow distortion, ultimately enabling the design of quieter, zero-emission aircraft. | ERC Consolid... | € 1.988.158 | 2024 | Details |
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.
Discovering novel control strategies for turbulent wings through deep reinforcement learning
DEEPCONTROL aims to enhance aviation sustainability by using deep reinforcement learning and high-fidelity simulations for real-time flow control around wings, reducing fuel consumption and emissions.
Acoustic fLow InteractioN over sound absorbing surfaces: effects on ImpedaNce and draG
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.
Linking the scales towards non-conventional polymer composite structures
The project aims to enhance aerospace composite structures by developing a systems-thinking methodology that integrates micro-scale studies with advanced analysis, unlocking new design potentials for efficiency.
MOdeling and Reduction of Aeroacoustics Sources of Interaction Noise in Aviation
The project aims to develop a holistic acoustic model for predicting interaction noise in aviation by understanding flow distortion, ultimately enabling the design of quieter, zero-emission aircraft.
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Pelican
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Bioinspired Electroactive Aeronautical multiscale LIVE-skin
The BEALIVE project develops a bio-inspired live skin for air-vehicles that enhances aerodynamic performance and reduces noise through advanced electroactive materials and real-time AI optimization.
DUWAAL hub & satellite Wieringerwerf
Het Duwaal Hub & Satellite-project demonstreert een geïntegreerde waardechain voor de productie en distributie van kosteneffectieve groene waterstof uit windenergie voor zero-emissie mobiliteit.
Project Puffin
Project Puffin ontwikkelt een pilot voor de Release Plant van LOHC-technologie, gericht op grootschalige waterstofopslag en -import, om de energietransitie te faciliteren en CO2-uitstoot te verminderen.