24 May 2023 U-HARWARD second dissemination event took place online on 24 May 2023. A total of 9 presentation were given from three inolved projects: five from the U-HARWARD, three from the REHA and one from the UP Wing. We were pleased to share the results with more than 50 attendees. All the presentations
May 2023 The first week of May, 2023, the flutter test of aeroelastic model AE1 has been successfully completed at POLIMI’s Large Wind tunnel. Different velocities, angles of attack as well as chordwise positions of the strut- wing connection have been successfully tested. The identification phase has been carried out combining an air jet
May 2023 The aeroelastic wind tunnel model named AE1 represents a constant Froude scaled model of the strut-braced wing configuration including both wing and structure. It is conceived for the preliminary low speed flutter investigations and for a limited number of sensitivity analysis. The model has been conceived by ONERA, POLIMI and IBK, while
THE PARTICIPATION TO THIS EVENT IS FREE: FOR ORGANIZATION REASONS IT IS REQUESTED A REGISTRATION. Register Here! ONLINE WORKSHOP Wednesday May 24, 2023: 9:00 - 13:00 Agenda U-HARWARD Project Contributions 9:00 – 9:20 Introduction, Project structure, methods, goals and status (POLIMI) 9:20 – 9:40 Conceptual and preliminary design of high aspect ratio
October 20, 2022 Two presentations have been given by U-HARWARD consortium covering the last achievements obtained recently during the project development.
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.
