Advanced Research Into Aeromechanical Solutions

Informazioni relative al progetto

ARIAS

ID dell’accordo di sovvenzione: 769346

DOI

10.3030/769346

Progetto chiuso

Data della firma CE 18 Maggio 2018

Data di avvio 1 Settembre 2018

Data di completamento 28 Febbraio 2023

Finanziato da

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Costo totale

€ 7 657 442,50

Contributo UE

€ 7 503 731,00

Coordinato da

KUNGLIGA TEKNISKA HOEGSKOLAN
Sweden

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

Websites, patent fillings, videos etc. (2)

Project web page

Project web-page published

ARIAS e-learning repository

This delivery will contain all the learning modules developed within the project

Documents, reports (5)

Summary of project results

Public report on main results and achievements of the project

Achievements of ARIAS project (review paper)

Review paper on project results

Workshop on turbomachinery aeromechanical design and analysis tools in the e-learning perspective

The delivery will include the program and the presentations of the workshop to be performed in connection with the 35 year meeting on the learning modules

Summary of project goals and objectives

Publish a summary of project goals and objectives on the project web page

Strategies for the implementation of acquired results into higher education

Establish the approach for most effective implementation of the project results into educational activities of academic partners

Pubblicazioni

Conference proceedings (13)

Numerical Investigation of Forced Response in a Transonic Compressor Stage – Highlighting Challenges Using Experimental Validation

Autori: Kilian,M., Klausmann, F., Franke, D., Schiffer, H-P., Gutiérrez Salas, M.
Pubblicato in: Proceedings of ISUAAAT16 Conference, Numero ISUAAAT16, Sept 2022, 2022, Pagina/e ISUAAAT16- 37
Editore: ISUAAAT16

Aeroelastic Response of a Transonic Compressor Cascade at High Reduced Frequencies

Autori: Glodic, N., Tavera Guerrero, C., Gutiérrez Salas, M.
Pubblicato in: Proceedings of ISUAAAT16 Conference, Numero ISUAAAT16, Sept 2022, 2022, Pagina/e "paper # ISUAAAT16- 35"
Editore: ISUAAAT16

Mistuning Effects on the Nonlinear Friction Saturation of Flutter Vibration Amplitude

Autori: Carlos Martel, Salvador Rodríguez
Pubblicato in: Volume 10A: Structures and Dynamics, 2020, ISBN 978-0-7918-8421-8
Editore: American Society of Mechanical Engineers
DOI: 10.1115/gt2020-15442

NONLINEAR FLUTTER ANALYSIS OF THE ZERO NODAL DIAMETER OF A LABYRINTH SEAL

Autori: RoqueCorral, MicheleGreco and J.LuisMatabuena
Pubblicato in: Proceedings of GPPS Xi'an 2021, Numero ISSN-Nr:2504-4400, 2021
Editore: GPPS Global

Development of a novel static seal flutter rig

Autori: Hualca, F., Schwingshackl, C., Setchfield, R., Gallego, J., Korte, D., Corral, R., Greco, M., Bermejo, O.
Pubblicato in: Proceedings of ISUAAAT16 Conference, Numero ISUAAAT16, Sept 2022, 2022, Pagina/e "paper # ISUAAAT16- 51"
Editore: ISUAAAT16

Experimental research into aeroelastic phenomena in turbine rotor blades inside ARIAS EU project

Autori: Gallardo, J. M., Bermejo, O., Hernández,J., García, G., J. Gallego, J., Knappett, D., Kharyton, V., Wurl, M., Corral, R.
Pubblicato in: Proceedings of ISUAAAT16 Conference, Numero ISUAAAT16, Sept 2022, 2022, Pagina/e "paper # ISUAAAT16- 30"
Editore: ISUAAAT16

Advanced Processing of a Blade Vibratory Response Obtained With Tip Timing Method Using Hyperparameter-Free Sparse Estimation Method

Autori: Vsevolod Kharyton, Dave Zachariah
Pubblicato in: Volume 9B: Structures and Dynamics — Fatigue, Fracture, and Life Prediction; Probabilistic Methods; Rotordynamics; Structural Mechanics and Vibration, 2021, ISBN 978-0-7918-8503-1
Editore: ASME
DOI: 10.1115/gt2021-02411

Blade oscillation mechanism for aerodynamic damping measurements at high reduced frequencies

Autori: Nenad Glodic, Carlos Tavera Guerrero, Mauricio Gutierrez Salas
Pubblicato in: Biennial Symposium on Measuring Techniques in Turbomachinery, Numero XXV, 2020
Editore: MTT2520

Experimental validation of a seal flutter model

Autori: Corral, R., Greco, M.
Pubblicato in: Proceedings of ISUAAAT16 Conference, Numero ISUAAAT16, Sept 2022, 2022, Pagina/e "paper # ISUAAAT16- 46"
Editore: ISUAAAT16

Numerical Validation of an Analytical Seal Flutter Model

Autori: Roque Corral, Michele Greco
Pubblicato in: Proceedings of Global Power & Propulsion Society, 2020
Editore: GPPS
DOI: 10.33737/gpps20-tc-142

Higher-Order Conceptual Model for Labyrinth Seal Flutter

Autori: Roque Corral, Michele Greco, Almudena Vega
Pubblicato in: Volume 10A: Structures and Dynamics, 2020, ISBN 978-0-7918-8421-8
Editore: American Society of Mechanical Engineers
DOI: 10.1115/gt2020-14387

Bringing Turbomachinery Aeromechanics Research Closer to Education

Autori: Glodic, N., Gutierrez Salas, M., Franke D., Tavera Guerrero, C., F. Klausmann,
Pubblicato in: Proceedings of ISUAAAT16 Conference, Numero ISUAAAT16, Sept 2022, 2022, Pagina/e "paper # ISUAAAT16- 43"
Editore: ISUAAAT16

Nonlinear mode interaction effects in the vibration of bladed-disks

Autori: Salvador Rodríguez, Carlos Martel
Pubblicato in: Proceedings of Global Power & Propulsion Society, 2020
Editore: GPPS
DOI: 10.33737/gpps20-tc-108

Peer reviewed articles (7)

Nonlinear switching between flutter and forced response in bladed disks

Autori: Javier González-Monge; Salvador Rodríguez-Blanco; Carlos Martel
Pubblicato in: Nonlinear dynamics, Numero vol.111, 2022, Pagina/e 5237–5247, ISSN 1573-269X
Editore: Springer
DOI: 10.1007/s11071-022-08140-9

Analysis of experimental results of turbomachinery flutter using an asymptotic reduced order model

Autori: Salvador Rodríguez, Carlos Martel
Pubblicato in: Journal of Sound and Vibration, Numero 509, 2021, Pagina/e 116225, ISSN 0022-460X
Editore: Academic Press
DOI: 10.1016/j.jsv.2021.116225

Nonlinear Flutter Analysis of Labyrinth Seals

Autori: Roque Corral, Michele Greco, Luis Matabuena
Pubblicato in: Journal of Turbomachinery, Numero Vol 145, issue 7, 2023, ISSN 1528-8900
Editore: ASME
DOI: 10.1115/1.4056701

Numerical Validation of an Analytical Seal Flutter Model

Autori: Michele Greco; Roque Corral
Pubblicato in: Journal Glob. Power Propuls. Soc. 2021, Numero vol 5, 2021, Pagina/e 191–201, ISSN 2515-3080
Editore: GPPS
DOI: 10.33737/jgpps/141210

Characterization of the Anomalous Vibration Response of an Intentionally Mistuned LPT Rotor

Autori: Salvador Rodríguez-Blanco; Carlos Martel
Pubblicato in: Machines, Numero Vol.11, Numero 1, 2023
Editore: MDPI
DOI: 10.3390/machines11010019

Effective Clearance and Differential Gapping Impact on Seal Flutter Modeling and Validation

Autori: Roque Corral, Michele Greco, Almudena Vega
Pubblicato in: Journal of Turbomachinery, Numero vol.144, issue 7, 2022, ISSN 1528-8900
Editore: ASME
DOI: 10.1115/1.4053290

Higher Order Conceptual Model for Labyrinth Seal Flutter

Autori: Roque Corral, Michele Greco, Almudena Vega
Pubblicato in: Journal of Turbomachinery, Numero Vol. 143 Numero 7, 2021, ISSN 1528-8900
Editore: ASME
DOI: 10.1115/1.4050334

Other (1)

ARIAS e-learning modules

Autori: Glodic, N., Tavera C., Gutierrez, M., Klausmann, F., Vogt, D.,Blanc, L.,D'Ettole, A.,Gallardo Antolin, .J. M.,Gallego-Garrido, J., Corral, R., Greco, M., Martel, C., Setchfield, R., Rodriguez, S.,Schwingshackl, C.
Pubblicato in: 2023
Editore: T.I.M.E. association learning repository