U-HARWARD
Financiado
Ultra High Aspect Ratio Wing Advanced Research and Designs
U-HARWARD will consider the use of innovative aerodynamic and aeroelastic designs in a multi-fidelity multi-disciplinary optimal design approach to facilitate the development of Ultra-High aspect ratio wings for large transport ai...
U-HARWARD will consider the use of innovative aerodynamic and aeroelastic designs in a multi-fidelity multi-disciplinary optimal design approach to facilitate the development of Ultra-High aspect ratio wings for large transport aircraft. A conceptual design study, building on the current state of the art, will perform trade-off studies to determine the potential gains of different wing configurations and loads alleviation concepts in terms of aerodynamics, weight, noise, fuel-burn and range. Scaled model wind tunnel tests will be used to validate parametric variations in the aerodynamic and acoustic characteristics. Starting from a reference aircraft, the preliminary design of the best candidate configuration will be completed and the estimated gains validated using high fidelity tools and a larger scale aeroelastic test.
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Duración del proyecto: 43 meses
Fecha Inicio: 2020-03-09
Fecha Fin: 2023-10-31
Fecha Fin: 2023-10-31
Línea de financiación: concedida
El organismo H2020 notifico la concesión del proyecto el día 2023-10-31
Línea de financiación objetivo
El proyecto se financió a través de la siguiente ayuda:
JTI-CS2-2019-CFP10-THT-07:
Ultra-High Aspect ratio wings
Cerrada
hace 5 años
Presupuesto
El presupuesto total del proyecto asciende a
3M€
Líder del proyecto
POLITECNICO DI MILANO
No se ha especificado una descripción o un objeto social para esta compañía.
Perfil tecnológico
TRL
4-5
Perfil tecnológico
TRL
4-5
229.52K€ |
Participante
133.00K€ |
Participante