Ultra High Aspect Ratio Wing Advanced Research and Designs

Leistungen

Aerodynamic (HQ - SBW configuration) test report

WT test report of aerodynamic test on AA model

Final report on the assessment of the impact on business and environment in terms of noise, NOx and CO2, of the optimized aircraft configurations

Report describing the assessment of the impact on business and environment in terms of noise NOx and CO2 of the optimized aircraft configurationsCONTRIBUTORSAll the partners will support UNIVBRIS in the final assessment phase of the technologies developed during the entire project

Aero-servo-elastic WT (FWT configuration) test report

WT test report of aerodynamic test on AE2 modelCONTRIBUTORSPOLIMI will be responsible of the finalization of the test reportIBK and UNIVBRIS will support POLIMI during the posttest analysis and correlation phases

Final report on impact analysis and development roadmap

Final Report containing the analysis on business and environmental impact and the roadmap to a successful deployment of the optimized UHARW configurationsCONTRIBUTORSAll the partners will support UNIVBRIS in the final definition of a possible roadmap for the most promising technologies

Dissemination, Communication and Exploitation Plan

Plan for dissemination and exploitation of project results (D). Contribution: (All the beneficiaries)

Aeroacoustic WT test report

Document reporting the results of the experimental campaign carried out at aeroacoustic wind tunnel of UNIVBRISCONTRIBUTORSUNIVBRIS will assess and collect the experimental aeroacoustic results SIEMENS will support the correlation and final assessment with the numerical HIFI simulation results of the tested configuration

High Fidelity aero-structural analysis for CNT and FWT configurations

Document reporting the HF aeroelastic analysis of cantilever wing configuration equipped with folding wingtip mechanismCONTRIBUTORSSIEMENS will perform the HIFI aerostructural analyses of the optimized folding wingtip configurations A special care will be devoted to the mechanical simulation of the folding mechanismUNIVBRIS will share the aeroelastic medium fidelity model of the optimized folding wingtip configurations and will support SIEMENSPOLIMI will support SIEMENS to derive the relevant results supporting the definition of the final aeroservoelastic wind tunnel model to be tested at POLIMI

Trade-off analysis of the HARW configurations and definition of the Wind Tunnel experimental campaign

Document comparing the performances of the different HARW configurations and supporting the definition of the experimental campaignThe document includes a tradeoff of the advanced HARW configurations and defined the number and configurations of wind tunnel models for the experimental validation CONTRIBUTORSUNIVBRIS will assess the results provided by the three teams working on the different configurations POLIMI will provide an overview of the different models and type of wind tunnel tests necessary to validate the results obtained from aerodynamic and aeroservoelastic point of view

Literature review and aircraft user-case definition

Report describing the literature study and the identification and aerodynamic reverse design of the aircraft reference

Definition of test objectives and requirements

Selection of the Wind Tunnel and Definition of test objectives and requirements. The document includes the target of the test, the description of the test setup to be provided including number and type of measurements, a preliminary test matrix. (contr. ONERA, UNIVBRIS, IBK)

High Fidelity aerodynamic and aero-acoustic analysis of SBW configuration

Document reporting the HIFI aeroacoustic analysis results of SBW configurationCONTRIBUTORSSIEMENS will perform the aeroacoustic HIFI analyses of wind tunnel aeroacoustic model to be tested at UNIVBRIS and of the SBW optimized configuration ONERA will contribute with the HIFI aerodynamic results of SBW optimized configuration as well as the results of sensitivity analyses

Preliminary design and comparison of end-user cases for CNT, S/TBW and FWT configurations

Document reporting the results of preliminary analysis of different HARW configurations as output of tasks 23 24 and 25This report summarizes the results obtained in the case of optimized aircraft in all the three configurations ie Cantilever SBW and Folding WingtipCONTRIBUTORSISAE will collect and summarize the results provided by POLIMIIBK ONERA and UNIVBRIS related to the results obtained for HARW cases for the configurations CNT SBW and FWT

Design, manufacturing, instrumentation, and delivery of WT model for aeroacoustic tests

Reports on the activity on design manufacturing and finalization of the aeroacoustics experimental campaign at UNIVBRIS acoustic wind tunnel

Aeroelastic WT model (SBW configuration) test report

WT test report of aeroelastic test on AE1 model

Methods and tools adopted and Reference Aircraft analysis results

Document describing the tools adopted their validation and the analysis results of Reference AircraftThis report describes the tools adopted by different partners and compares the results obtained in the case of CeRAS data base and of Reference AircraftCONTRIBUTORSPOLIMIIBK will provide the description of NeoCASS tool including the new module for emissions calculation together with the results of CeRAS and Reference Aircraft casesONERAIISAE will provide the description of updated FastOAD tool together with the results of CeRAS and Reference Aircraft casesUNIVBRIS will provide the description of suite ALENA together with the results of CeRAS and Reference Aircraft cases

Data Management Plan

This report addresses the relevant aspects of making data findable, accessible, interoperable and re-usable, including what data the project will generate, whether and how it will be made accessible for verification and re-use, and how it will be curated and preserved. This deliverable allows to participate in the Open Research Data Pilot

Design, manufacturing, instrumentation, and delivery of WT model for aeroelastic test (SBW configuration)

Complete description and delivery of WT model AE1.CONTRIBUTORS:IBK will provide the final mechanical design of the aeroelastic wind tunnel model (SBW configuration) and its connections to the POLIMI’s wind tunnel and will coordinate the manufacturing process (subco).POLIMI will provide the preliminary design of the model, including the scaling process, as well as the final installation of the instrumentation.

Veröffentlichungen

A THT Project Aiming at Ultra High Aspect Ratio Wings Advanced Research and DesignsS

Autoren: Sergio Ricci
Veröffentlicht in: 2021
Herausgeber: n/a
DOI: 10.5281/zenodo.5145447

Multidisciplinary analysis and design of strut-braced wing concept for medium range aircraft

Autoren: Gerald G. Carrier, Guillaume Arnoult, Nicolo Fabbiane, Jean-Sebastien Schotte, Christophe David, Sébastien Defoort, Emmanuel Benard and Martin Delavenne
Veröffentlicht in: AIAA SCITECH 2022 Forum, Ausgabe 1, 2022
Herausgeber: AIAA
DOI: 10.2514/6.2022-0726

Sizing of High Aspect Ratio Wings with Folding Wing Tips

Autoren: Huaiyuan Gu, Fintan Healy, Djamel Rezgui and Jonathan E. Cooper
Veröffentlicht in: AIAA SCITECH 2022 Forum, Ausgabe 1, 2022
Herausgeber: AIAA
DOI: 10.2514/6.2022-0723

Aero-Servo-Elastic Optimization in Early Design Phases

Autoren: Toffol, F.; Ricci, S.
Veröffentlicht in: AIDAA - XXVI INTERNATIONAL CONGRESS 31ST AUGUST – 3 RD SEPTEMBER 2021, Ausgabe 1, 2021
Herausgeber: AIDAA

Non-Linear Aeroelastic Capabilities in NeoCASS Suite

Autoren: Toffol, F.;Fonzi, N.;Ricci, S.
Veröffentlicht in: AIAA Scitech 2023 Forum, Ausgabe AIAA 2023-2406, 2023, Seite(n) 1-15
Herausgeber: AIAA
DOI: 10.2514/6.2023-2406

Recent Achievements in the Design of Ultra High Aspect Ratio Wings of Environmental Friendly Aircraft

Autoren: Ricci Sergio
Veröffentlicht in: 2021
Herausgeber: IOP Publishing Ltd
DOI: 10.5281/zenodo.5706398

U-HARWARD Final Dissemination Event

Autoren: Many
Veröffentlicht in: AR20+: Workshop on High Aspect Ratio Wing Technologies: Session 7, U-HARWARD Final Dissemination Event, 2023
Herausgeber: Imperial College
DOI: 10.52843/cassyni.wtyr92

U‐HARWARD: a CS2 EU funded project aiming at the Design of Ultra High Aspect Ratio Wings Aircraft

Autoren: S.Ricci
Veröffentlicht in: 3rd European Workshop on MDO for industrial applications in aeronautics, toward greener aviation, Ausgabe Annual, 2022
Herausgeber: Onera

Multi-fidelity weight analyses for high aspect ratio strut-braced wings preliminary design

Autoren: M Delavenne, E Benard, S Defoort, C David, N Fabbiane, J S Schotte, G Arnoult and G Carrier
Veröffentlicht in: IOP Conference Series: Materials Science and Engineering, Ausgabe 1226 012009, 2022, ISSN 1757-899X
Herausgeber: IOP
DOI: 10.1088/1757-899x/1226/1/012009

Aeroelastic Optimization of High Aspect Ratio Wings for Environmentally Friendly Aircraft

Autoren: Ricci, S.; Marchetti, L.; Toffol, F.; Beretta, J.; Paletta, N.
Veröffentlicht in: AIAA SCITECH 2022 Forum, Ausgabe 1, 2022
Herausgeber: AIAA
DOI: 10.2514/6.2022-0166

U-HARWARD Second Dissemination Event

Autoren: Many
Veröffentlicht in: U-HARWARD Second Dissemination Event, 2023
Herausgeber: U-HARWARD

Overview of Aerodynamic Design Activities Performed at ONERA to Reduce Aviation's Climate Impact 1

Autoren: Méheut, Michaël; Arnoult, Guillaume; Atinault, Olivier; Bennehard, Quentin; François, Christophe
Veröffentlicht in: 33rd ICAS Congress, Ausgabe 1, 2022
Herausgeber: ICAS

AEROELASTIC ANALYSIS AND OPTIMIZATION OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS

Autoren: Le Lamer, Yoann; Morlier, Joseph; Bénard, Emmanuel; He, Ping
Veröffentlicht in: AEROELASTIC ANALYSIS AND OPTIMIZATION OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS. AEROBEST (Thematic Conference on Multidisciplinary Design Optimization of Aerospace Systems ),, Ausgabe 1, 2023
Herausgeber: IDMEC

U-HARWARD: a CS2 EU Funded Project Aiming at the Design of Ultra High Aspect Ratio Wings Aircraft

Autoren: Ricci, S.; Paletta, N.; Defoort, S.; Benard, E.; Cooper, J. E.; Barabinot, P.
Veröffentlicht in: AIAA SCITECH 2022 Forum, Ausgabe 1, 2022
Herausgeber: AIAA
DOI: 10.2514/6.2022-0168

Wingbox Meta-Model and Aero-Servo-Elastic Optimization With NEOPT

Autoren: Toffol, F.; Ricci, S.
Veröffentlicht in: AeroBest 2021 Lisboa, 21-23 July 2021, Ausgabe 2, 2021, ISBN 978-989-99424-8-6
Herausgeber: IDMEC

DESIGN OF A WIND TUNNEL MODEL FOR FLUTTER INVESTIGATION OF STRUT-BRACED HIGH ASPECT RATIO WING IN THE FRAMEWORK OF CS2-THT U-HARWARD PROJECT

Autoren: Toffol, F
Veröffentlicht in: 12th EASN International Conference, Ausgabe 4, 2022
Herausgeber: EASN
DOI: 10.5281/zenodo.10533765

A THT Project Aiming at Ultra High Aspect Ratio Wings Advanced Research and DesignsS

Autoren: Sergio Ricci
Veröffentlicht in: "11th EASN International Conference on ""Innovation in Aviation & Space for opening New Horizons""", Ausgabe 1, 2021
Herausgeber: EASN

CS2-THT U-HARWARD PROJECT: RECENT ACHIEVEMENTS IN THE DESIGN OF ULTRA HIGH ASPECT RATIO WINGS

Autoren: Ricci, Sergio
Veröffentlicht in: 12th EASN International Conference, Ausgabe 1, 2022
Herausgeber: EASN
DOI: 10.5281/zenodo.10533690

Sizing of High Aspect Ratio Wing incorporating Folding Wingtips

Autoren: Huaiyuan Gu, Fintan Healy, Jonathan Cooper
Veröffentlicht in: 2021, ISBN 978-989-99424-8-6
Herausgeber: IDMEC Instituto Superior Técnico Universidade de Lisboa
DOI: 10.5281/zenodo.5708286

Sizing of High-Aspect-Ratio Wings with Folding Wingtips

Autoren: Huaiyuan Gu; Fintan Healy; Djamel Rezgui; Jonathan Cooper
Veröffentlicht in: Journal of Aircraft, Ausgabe 60, 2023, ISSN 1533-3868
Herausgeber: AIAA
DOI: 10.2514/1.c036908

Preliminary Aero-Elastic Optimization of a Twin-Aisle Long-Haul Aircraft with Increased Aspect Ratio

Autoren: Francesco Toffol; Sergio Ricci
Veröffentlicht in: Aerospace; Volume 10; Ausgabe 4; Pages: 374, Ausgabe 1, 2023, ISSN 2226-4310
Herausgeber: mdpi
DOI: 10.3390/aerospace10040374

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