Development of innovative FunctiOnal aiRcraft MOveable SurfAces

Project Information

FORMOSA

Grant agreement ID: 885971

DOI 10.3030/885971

Project closed

EC signature date 23 March 2020

Start date 1 September 2020

End date 28 February 2023

Funded under

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Total cost € 500 000,00

EU contribution € 500 000,00

Coordinated by

POLITECNICO DI MILANO
Italy

Deliverables

Documents, reports (2)

Communication, Dissemination & Exploitation Report

Reports describing the activities carried out during the project to promote awareness of project results and to exploit project resultsContributions POLIMI CEIA

Dissemination, comunication and Exploiation Plan

Report describing the intended activities to be carried out for dissemination Comunication and exploitation of projects resultsPresentation of the project websiteContributions POLIMI CEIA

Open Research Data Pilot (1)

Data Management Plan

ORDP Data Management PlanContributions POLIMI CEIA

Publications

Conference proceedings (7)

Development of Innovative Movable Surfaces for the Next-Generation Civil Tiltrotor Aircraft

Author(s): Savino, A.; Cardoso, J.; Pecoraro, M.; Muscarello, V.
Published in: Issue 1, 2023
Publisher: 20th Australian International Aerospace Congress

Mid-Fidelity Numerical Approach to Tiltrotor Aerodynamics

Author(s): Zanotti, A.; Savino, A.; Palazzi, M.; Tugnoli, M.; Muscarello, V.
Published in: 47th European Rotorcraft Forum (ERF 2021), Issue 1, 2021
Publisher: 47th European Rotorcraft Forum (ERF 2021)

Coupled multibody-mid fidelity aerodynamic solver for tiltrotor aeroelastic simulation

Author(s): A. Cocco, A. Savino, A. Zanotti, A. Zanoni, P. Masarati, and V. Muscarello
Published in: 9th International Conference on Computational Methods for Coupled Problems in Science and Engineering, COUPLED PROBLEMS 2021. CIMNE, 2021
Publisher: 9th International Conference on Computational Methods for Coupled Problems in Science and Engineering, COUPLED PROBLEMS 2021. CIMNE

Design and Optimization of Innovative Tiltrotor Wing Control Surfaces Through Coupled Multibody - Mid-Fidelity Aerodynamics Simulations

Author(s): Savino, A.; Cocco, A.; Zanoni, A.; De Gaspari, A.; Zanotti, A.; Cardoso, J.; Carvalhais, D.; Muscarello, V.
Published in: Issue 1, 2022
Publisher: 78th International Annual Forum Vertical Flight Society

A Coupled Multibody - Mid Fidelity Aerodynamic Tool for the Simulation of Tiltrotor Manoeuvres

Author(s): Savino, A.; Cocco, A.; Zanoni, A.; Zanotti, A.; Muscarello, V.
Published in: 47th European Rotorcraft Forum (ERF 2021), Issue 1, 2021
Publisher: 47th European Rotorcraft Forum (ERF 2021)

Numerical investigation of wing-propeller aerodynamic interaction through a vortex particle-based aerodynamic solver

Author(s): A. Savino, A. Cocco, A. Zanoni, and V. Muscarello
Published in: 48th European Rotorcraft Forum (ERF 2022), 2022
Publisher: 48th European Rotorcraft Forum (ERF 2022)

Simulation of Tiltrotor Maneuvers by a Coupled Multibody-Mid Fidelity Aerodynamic Solver

Author(s): Cocco, A.; ALBERTO SAVINO; Montagnani, D.; Tugnoli, M.; Guerroni, F.; Palazzi, M.; Zanoni, A.; Zanotti, A.; Muscarello, V.
Published in: 46th European Rotorcraft Forum (ERF 2020), Moscow, Russia, 8-11 Sept. 2020, Issue 1, 2020
Publisher: Russian Helicopters

Peer reviewed articles (2)

Assessment of a Mid-Fidelity Numerical Approach for the Investigation of Tiltrotor Aerodynamics

Author(s): Alex Zanotti, Alberto Savino, Michele Palazzi, Matteo Tugnoli, Vincenzo Muscarello
Published in: Applied Sciences, Issue 11/8, 2021, Page(s) 3385, ISSN 2076-3417
Publisher: Basel: Molecular Diversity Preservation International
DOI: 10.3390/app11083385

Coupling Mid-Fidelity Aerodynamics and Multibody Dynamics for the Aeroelastic Analysis of Rotary-Wing Vehicles

Author(s): Alberto Savino; Alessandro Cocco; Alex Zanotti; Matteo Tugnoli; Pierangelo Masarati; Vincenzo Muscarello
Published in: Energies, Vol 14, Iss 6979, p 6979 (2021), Issue 1, 2021, ISSN 1996-1073
Publisher: Multidisciplinary Digital Publishing Institute (MDPI)
DOI: 10.3390/en14216979