September 2022 The aeroacoustic tests on the flapped wing section model equipped with a representative strut has been successfully completed by UNIVBRIS at the aeroacoustic wind tunnel available at University of Bristol. The relevant results will support the final project assessment.
September 20, 2022 The Coordinator of U-HARWARD was invited to present the project at 3rd European Workshop on MDO on Industrial Applications in Aeronautics – Toward Greener Aviation, organized by ONERA, DLR and IRT Saint-Exupéry at in IHES - Paris (Bures-sur-Yvette) September 2022. During the workshop ONERA presented some recent results achieved under the
July 2022 The mechanical design of the wind tunnel model named AE1 has been completed by IBK. The model is composed by the wing plus the strut and will be tested at POLIMI’s Large Wind Tunnel facility for flutter investigation. It is an aeroelastic model, constant Froude scaled by POLIMI with respect to the
January 22, 2022 Three presentations have been given by U-HARWARD consortium during 2022 AIAA SCITECH FORUM held in San Diego, CA, 3-7 January 2022, in a Clean Aviation Special Session: Advanced Aircraft Concepts and Configurations
June 11th, 2021 Project U-HARWARD, Ultra High Aspect Ratio Wing Advanced Research and Designs successfully passed the Project Assessment review meeting at the end of First Reporting Period.
Project U-HARWARD, Ultra High Aspect Ratio Wing Advanced Research and Designs, in response to the topic JTI-CS2-2019-CFP10-THT-07, aims to facilitate the development of Ultra-High aspect ratio wings for medium and large transport aircraft by the use of innovative aerodynamic and aeroelastic designs in a multi-fidelity multi-disciplinary optimal design approach. During the kick-off meeting the
The Coordinator of U-HARWARD was invited to present the project in a dedicated session to illustrate the winners of the 2020 THT calls. U-HARWARD project, in response to the call JTI-CS2-2019-CFP10-THT-07: Ultra-High Aspect ratio wings, will consider the use of innovative aerodynamic and aeroelastic designs in a multi-fidelity multi-disciplinary optimal design approach to facilitate