CORDIS fornisce collegamenti ai risultati finali pubblici e alle pubblicazioni dei progetti ORIZZONTE.
I link ai risultati e alle pubblicazioni dei progetti del 7° PQ, così come i link ad alcuni tipi di risultati specifici come dataset e software, sono recuperati dinamicamente da .OpenAIRE .
Risultati finali
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 configurationsReport 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 reportWT 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 roadmapFinal 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 PlanPlan for dissemination and exploitation of project results (D). Contribution: (All the beneficiaries)
Aeroacoustic WT test reportDocument 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 configurationsDocument 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 campaignDocument 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 definitionReport describing the literature study and the identification and aerodynamic reverse design of the aircraft reference
Definition of test objectives and requirementsSelection 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 configurationDocument 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 configurationsDocument 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 testsReports on the activity on design manufacturing and finalization of the aeroacoustics experimental campaign at UNIVBRIS acoustic wind tunnel
Aeroelastic WT model (SBW configuration) test reportWT test report of aeroelastic test on AE1 model
Methods and tools adopted and Reference Aircraft analysis resultsDocument 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
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
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.
Pubblicazioni
Autori:
Sergio Ricci
Pubblicato in:
2021
Editore:
n/a
DOI:
10.5281/zenodo.5145447
Autori:
Gerald G. Carrier, Guillaume Arnoult, Nicolo Fabbiane, Jean-Sebastien Schotte, Christophe David, Sébastien Defoort, Emmanuel Benard and Martin Delavenne
Pubblicato in:
AIAA SCITECH 2022 Forum, Numero 1, 2022
Editore:
AIAA
DOI:
10.2514/6.2022-0726
Autori:
Huaiyuan Gu, Fintan Healy, Djamel Rezgui and Jonathan E. Cooper
Pubblicato in:
AIAA SCITECH 2022 Forum, Numero 1, 2022
Editore:
AIAA
DOI:
10.2514/6.2022-0723
Autori:
Toffol, F.; Ricci, S.
Pubblicato in:
AIDAA - XXVI INTERNATIONAL CONGRESS 31ST AUGUST – 3 RD SEPTEMBER 2021, Numero 1, 2021
Editore:
AIDAA
Autori:
Toffol, F.;Fonzi, N.;Ricci, S.
Pubblicato in:
AIAA Scitech 2023 Forum, Numero AIAA 2023-2406, 2023, Pagina/e 1-15
Editore:
AIAA
DOI:
10.2514/6.2023-2406
Autori:
Ricci Sergio
Pubblicato in:
2021
Editore:
IOP Publishing Ltd
DOI:
10.5281/zenodo.5706398
Autori:
Many
Pubblicato in:
AR20+: Workshop on High Aspect Ratio Wing Technologies: Session 7, U-HARWARD Final Dissemination Event, 2023
Editore:
Imperial College
DOI:
10.52843/cassyni.wtyr92
Autori:
S.Ricci
Pubblicato in:
3rd European Workshop on MDO for industrial applications in aeronautics, toward greener aviation, Numero Annual, 2022
Editore:
Onera
Autori:
M Delavenne, E Benard, S Defoort, C David, N Fabbiane, J S Schotte, G Arnoult and G Carrier
Pubblicato in:
IOP Conference Series: Materials Science and Engineering, Numero 1226 012009, 2022, ISSN 1757-899X
Editore:
IOP
DOI:
10.1088/1757-899x/1226/1/012009
Autori:
Ricci, S.; Marchetti, L.; Toffol, F.; Beretta, J.; Paletta, N.
Pubblicato in:
AIAA SCITECH 2022 Forum, Numero 1, 2022
Editore:
AIAA
DOI:
10.2514/6.2022-0166
Autori:
Many
Pubblicato in:
U-HARWARD Second Dissemination Event, 2023
Editore:
U-HARWARD
Autori:
Méheut, Michaël; Arnoult, Guillaume; Atinault, Olivier; Bennehard, Quentin; François, Christophe
Pubblicato in:
33rd ICAS Congress, Numero 1, 2022
Editore:
ICAS
Autori:
Le Lamer, Yoann; Morlier, Joseph; Bénard, Emmanuel; He, Ping
Pubblicato in:
AEROELASTIC ANALYSIS AND OPTIMIZATION OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS. AEROBEST (Thematic Conference on Multidisciplinary Design Optimization of Aerospace Systems ),, Numero 1, 2023
Editore:
IDMEC
Autori:
Ricci, S.; Paletta, N.; Defoort, S.; Benard, E.; Cooper, J. E.; Barabinot, P.
Pubblicato in:
AIAA SCITECH 2022 Forum, Numero 1, 2022
Editore:
AIAA
DOI:
10.2514/6.2022-0168
Autori:
Toffol, F.; Ricci, S.
Pubblicato in:
AeroBest 2021 Lisboa, 21-23 July 2021, Numero 2, 2021, ISBN 978-989-99424-8-6
Editore:
IDMEC
Autori:
Toffol, F
Pubblicato in:
12th EASN International Conference, Numero 4, 2022
Editore:
EASN
DOI:
10.5281/zenodo.10533765
Autori:
Sergio Ricci
Pubblicato in:
"11th EASN International Conference on ""Innovation in Aviation & Space for opening New Horizons""", Numero 1, 2021
Editore:
EASN
Autori:
Ricci, Sergio
Pubblicato in:
12th EASN International Conference, Numero 1, 2022
Editore:
EASN
DOI:
10.5281/zenodo.10533690
Autori:
Huaiyuan Gu, Fintan Healy, Jonathan Cooper
Pubblicato in:
2021, ISBN 978-989-99424-8-6
Editore:
IDMEC Instituto Superior Técnico Universidade de Lisboa
DOI:
10.5281/zenodo.5708286
Autori:
Huaiyuan Gu; Fintan Healy; Djamel Rezgui; Jonathan Cooper
Pubblicato in:
Journal of Aircraft, Numero 60, 2023, ISSN 1533-3868
Editore:
AIAA
DOI:
10.2514/1.c036908
Autori:
Francesco Toffol; Sergio Ricci
Pubblicato in:
Aerospace; Volume 10; Numero 4; Pages: 374, Numero 1, 2023, ISSN 2226-4310
Editore:
mdpi
DOI:
10.3390/aerospace10040374
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