Regional Aircraft

CORDIS fournit des liens vers les livrables publics et les publications des projets HORIZON.

Les liens vers les livrables et les publications des projets du 7e PC, ainsi que les liens vers certains types de résultats spécifiques tels que les jeux de données et les logiciels, sont récupérés dynamiquement sur OpenAIRE .

Livrables

DMP for Scientific Paper with underlined data shown in it

Data Management Plan for Year 2019 GAM Amdt – Art. 29.2

Synthesis of Air Vehicle Technologies first assessment at A/C level (Linked to 2018-D_2.1.4-19)

Progress report on energy saving evaluations about innovative process to replace hard chrome surface treatments (Linked to 2018-D_4.2-01)
On-Board Systems Progress Status Report 2018 (Linked to 2018-D_2.3-04)
Summary Report on Assessment of aero new devices against WTT results (Linked to 2019-D_3.5.1-01)
Coordination Memo on completion of drawings release for CDR of Full-scale Morphing Winglet Ground Demonstrator (Linked to 2018-D_2.1.2-22)

Coordination Memo on completion of drawings release for CDR of Full-scale Morphing Winglet Ground Demonstrator (Linked to 2018-D_2.1.2-22)

Summary Report of Safety assesment (rear engine mounting installation) -- Loop 2 (Linked to 2018-D_1.1.1-48)
Summary Report of WL/WT PDR (Linked to 2018-D_2.4.2-01)

Summary Report of WL/WT PDR (Linked to 2018-D_2.4.2-01)

Summary Report of Innovative configuration performance assesment - Loop 2 (Linked to 2018-D_1.1.1-43) (Linked to 2018-D_1.1.1-43)
Coordination Memo about release of Technical documentation supporting CDR of Centre Wing Assembly (MTP) (Linked to 2018-D_3.5.4-03)
Summary report on FCS EMA Interface Control, Performance and Design Document for WL/WT (Linked to 2018-D_2.4.2-17)
Coordination Memo on completion of drawings release for CDR of Full-scale Innovative Wing Tip Ground Demonstrator (Linked to 2018-D_2.1.2-24)

Coordination Memo on completion of drawings release for CDR of Full-scale Innovative Wing Tip Ground Demonstrator (Linked to 2018-D_2.1.2-24)

"Coordination Memo ""Innovative configuration, engine dataset -- loop 2"" (Linked to 2018-D_1.1.2-03)"

"Coordination Memo ""Innovative configuration, engine dataset -- loop 2"" (Linked to 2018-D_1.1.2-03) "

Coordination Memo about release of Technical documentation supporting CDR for Central Wingbox (Linked to 2018-D_3.5.1-03)
Summary Report of IVHM framework description (Linked to 2018-D_2.2.3-07)
REG IADP Dissemination and Exploitation Management Plan (Linked to D_0.5-02)

Updating of REG IADP results dissemination and exploitation plan, register included

Dissemination and Exploitation Management Plan (Updating) (Linked to 2018-D_0.5-01)
Coordination Memo: OWB F/S, R/S and Ribs Drawings release (Linked to 2018-D_3.1.3-01)

Coordination Memo: OWB F/S, R/S and Ribs Drawings release (Linked to 2018-D_3.1.3-01)

REG IADP risks management plan (Linked to D_0.3-02)

Updating of REG IADP risks management plan, register included

"Coordination Memo ""E-LGS Final Design"" (Linked to 2018-D_2.3.2-12)"
Summary Report on Predictive geometries for the Assembly of FTB2 (Linked to 2018-D_3.5.4-01)
Coordination Memo: OWB Stiffened Panels drawings release (Linked to 2018-D_3.1.3-02)
Final Winglet/Wingtip EMA Specification Summary

Final Winglet/Wingtip EMA Specification (Linked to O2.4.1-07 and O2.4.1-08)

Coordination Memo abourt release of Technical documentation supporting CDR (Linked to 2018-D_3.5.3-01)
Coordination Memo: Release of the Innovative ECS Recirculation/Air Treatment System Specification (Linked to KO_2.3.3-07)

System specification input for CfP

Publications

Design of a wing tip device for active maneuver and gust load alleviation

Auteurs: Federico Fonte, Francesco Toffol, Sergio Ricci
Publié dans: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, ISBN 978-1-62410-532-6
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-1442

PARAMETRIC APPROACH TO OPERATING COSTS ESTIMATION FOR AN INNOVATIVE REGIONAL AIRCRAFT

Auteurs: M. Fioriti*, N. Viola*, D. Ferretto*, V. Vercella* and S. Cresto Aleina* *Department of Mechanical and Aerospace Engineering - Politecnico di Torino F. Nicolosi† and V. Cusati† †Department of Industrial Engineering – Aerospace division University of Naples Federico II
Publié dans: 2018
Éditeur: ICAS

Effects of riblets on the performances of a regional aircraft configuration in NLF conditions

Auteurs: Pietro Catalano, Donato de Rosa, Benedetto Mele, Renato Tognaccini, Frederic Moens
Publié dans: 2018 AIAA Aerospace Sciences Meeting, 2018, ISBN 978-1-62410-524-1
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-1260

Design of a Leading Edge Morphing Based on Compliant Structures for a Twin-Prop Regional Aircraft

Auteurs: Sergio Ricci, Alessandro De Gaspari, Alessandro Gilardelli, Alessandro Airoldi
Publié dans: 2018 AIAA/AHS Adaptive Structures Conference, 2018, ISBN 978-1-62410-531-9
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-1063

Hybrid guided wave based SHM system for composite structures for impact and delamination detection combining fiber Bragg grating sensing and piezoelectric patches

Auteurs: Ernesto Monaco, Natalino Daniele Boffa, Leandro Maio, Fabrizio Ricci, Edgar Mendoza, Tribikram Kundu, Vittorio Memmolo
Publié dans: Health Monitoring of Structural and Biological Systems XII, 2018, Page(s) 12, ISBN 9781-510616974
Éditeur: SPIE
DOI: 10.1117/12.2297694

Performance evaluation and DOC Estimation of an Innovative Turboprop Configuration

Auteurs: Fabrizio Nicolosi, Salvatore Corcione, Vittorio Trifari, Vincenzo Cusati, Manuela Ruocco, Pierluigi Della Vecchia
Publié dans: 2018 Aviation Technology, Integration, and Operations Conference, 2018, ISBN 978-1-62410-556-2
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3662

Thrust Extraction from Vorticity Fields in Steady and Unsteady Flows

Auteurs: Lorenzo Russo, Mario Ostieri, Renato Tognaccini
Publié dans: 2018 Applied Aerodynamics Conference, 2018, ISBN 978-1-62410-559-3
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3967

The relation between vorticity-based and thermodynamic-based drag breakdown

Auteurs: L. L. Kang∗ , J. Z. Wu∗ , L. Russo† , R. Tognaccini†
Publié dans: 2018
Éditeur: TU Wien/ EUROMECH

“Aerodynamic design and analysis of an innovative regional turboprop configuration”

Auteurs: Fabrizio Nicolosi*, Salvatore Corcione*, Pierluigi Della Vecchia*, Vittorio Trifari*, Manuela Ruocco*, *University of Naples Federico II, Department of Industrial Engineering, Aerospace Division
Publié dans: 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018,, 2018
Éditeur: ICAS

Multi-Modal Morphing Wing Flaps for Next Generation Green Regional Aircraft: The CleanSky Challenge

Auteurs: Rosario Pecora
Publié dans: Volume 1: Development and Characterization of Multifunctional Materials; Modeling, Simulation, and Control of Adaptive Systems; Integrated System Design and Implementation, 2018, Page(s) V001T04A018, ISBN 978-0-7918-5194-4
Éditeur: ASME
DOI: 10.1115/smasis2018-8108

Control strategy of an electrically actuated morphing flap for the next generation green regional aircraft

Auteurs: Maurizio Arena, Maria Chiara Noviello, Francesco Rea, Francesco Amoroso, Rosario Pecora
Publié dans: Active and Passive Smart Structures and Integrated Systems XII, 2018, Page(s) 19, ISBN 9781-510616875
Éditeur: SPIE
DOI: 10.1117/12.2296424

Feasibility studies for the installation of Plasma Synthetic Jet Actuators on the skin of a morphing wing flap

Auteurs: Maurizio Arena, Matteo Chiatto, Francesco Amoroso, Rosario Pecora, Luigi de Luca
Publié dans: Active and Passive Smart Structures and Integrated Systems XII, 2018, Page(s) 21, ISBN 9781-510616875
Éditeur: SPIE
DOI: 10.1117/12.2300512

Aeroelastic stability analysis of a large civil aircraft equipped with morphing winglets and adaptive flap tabs

Auteurs: Rosario Pecora, Francesco Amoroso, Ignazio Dimino, Antonio Concilio, Maria Chiara Noviello
Publié dans: Active and Passive Smart Structures and Integrated Systems XII, 2018, Page(s) 20, ISBN 9781-510616875
Éditeur: SPIE
DOI: 10.1117/12.2300173

Preliminary Assessment of Morphing Winglet and Flap Tabs Influence on the Aeroelastic Stability of Next Generation Regional Aircraft

Auteurs: Maria Chiara Noviello, Ignazio Dimino, Francesco Amoroso, Antonio Concilio, Rosario Pecora
Publié dans: Volume 1: Development and Characterization of Multifunctional Materials; Modeling, Simulation, and Control of Adaptive Systems; Integrated System Design and Implementation, 2018, Page(s) V001T04A020, ISBN 978-0-7918-5194-4
Éditeur: ASME
DOI: 10.1115/smasis2018-8138

Technological demonstration of an adaptive aileron system

Auteurs: Gianluca Amendola, Ignazio Dimino, Rosario Pecora, Francesco Amoroso, Leonardo Lecce, Antonio Concilio
Publié dans: Bioinspiration, Biomimetics, and Bioreplication VIII, 2018, Page(s) 3, ISBN 9781-510616837
Éditeur: SPIE
DOI: 10.1117/12.2297083

AIRGREEN2 - Clean Sky 2 Programme: Adaptive Wing Technology Maturation, Challenges and Perspectives

Auteurs: Salvatore Ameduri, Antonio Concilio, Ignazio Dimino, Rosario Pecora, Sergio Ricci
Publié dans: Volume 1: Development and Characterization of Multifunctional Materials; Modeling, Simulation, and Control of Adaptive Systems; Integrated System Design and Implementation, 2018, Page(s) V001T04A023, ISBN 978-0-7918-5194-4
Éditeur: ASME
DOI: 10.1115/smasis2018-8235

Piezo-driven and Plasma Synthetic Jet Actuators. A comparative investigation

Auteurs: Chiatto M., Palumbo A., De Luca, L
Publié dans: 2018
Éditeur: GWFMD

Structural Design of a Multifunctional Morphing Fowler Flap for a Twin-Prop Regional Aircraft

Auteurs: Francesco Rea, Francesco Amoroso, Rosario Pecora, Maria Chiara Noviello, Maurizio Arena
Publié dans: Volume 1: Development and Characterization of Multifunctional Materials; Modeling, Simulation, and Control of Adaptive Systems; Integrated System Design and Implementation, 2018, Page(s) V001T04A003, ISBN 978-0-7918-5194-4
Éditeur: ASME
DOI: 10.1115/smasis2018-7937

Design of an Adaptive Twist Trailing Edge for Large Commercial Aircraft Applications

Auteurs: Francesco Rea, Francesco Amoroso, Rosario Pecora, Markus Kintscher
Publié dans: Volume 1: Development and Characterization of Multifunctional Materials; Modeling, Simulation, and Control of Adaptive Systems; Integrated System Design and Implementation, 2018, Page(s) V001T04A004, ISBN 978-0-7918-5194-4
Éditeur: ASME
DOI: 10.1115/smasis2018-7939

Design and aerodynamic analysis of a regional turboprop innovative configuration

Auteurs: Nicolosi F., Corcione S., Della Vecchia P., Trifari V., Ruocco M., De Marco A.
Publié dans: Paper 893, 6th CEAS Conference , CEAS2017,, 2017, ISBN 978-973-0-25597-3
Éditeur: CEAS

Developing of a Simscape Multibody Contact Library for Gothic Arc Ball Screws: A Three-Dimensional Model for Internal Sphere/Grooves Interactions

Auteurs: Antonio Carlo Bertolino, Giovanni Jacazio, Stefano Mauro, Massimo Sorli
Publié dans: Volume 4: Dynamics, Vibration, and Control, 2019, ISBN 978-0-7918-5941-4
Éditeur: American Society of Mechanical Engineers
DOI: 10.1115/imece2019-10709

Robust Design of a Test Bench for PHM Study of Ball Screw Drives

Auteurs: A. C. Bertolino, A. De Martin, G. Jacazio, S. Mauro, M. Sorli
Publié dans: Volume 1: Advances in Aerospace Technology, 2019, ISBN 978-0-7918-5936-0
Éditeur: American Society of Mechanical Engineers
DOI: 10.1115/imece2019-10713

Electrical Flight Control for load control and alleviation system

Auteurs: G.Pozzuto, A. De Martin, G.Pispola, M. Palmieri, F.Gallorini
Publié dans: MEA2019 Conferences, 2019
Éditeur: MEA2019 Conferences

“Surrogate Models in flap design of Clean Sky 2”

Auteurs: S.de Lucas
Publié dans: EUROGEN 2019 Portugal, Numéro Bi-yearly, 2019
Éditeur: EUROGEN: Evolutionary and Deterministic Computing for Industrial Applications within EUCCOMAS

"“Inclusion of structure and loads objectives in the definition of probability for Flight Control System failures in the frame of FTB#2 Cleansky2”"

Auteurs: M.Rodriguez
Publié dans: EuCASS 2019 Spain, Numéro Bi-yearly, 2019
Éditeur: EuCASS: 8th European Conference for Aeronautics and Space Sciences

Design Guidelines for High Capacity Innovative Regional Turboprop Aircraft

Auteurs: Fabrizio Nicolosi, Salvatore Corcione, Vittorio Trifari, Pierluigi Della Vecchia, Agostino De Marco
Publié dans: AIAA Scitech 2019 Forum, 2019, ISBN 978-1-62410-578-4
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-0256

Green regional aircraft gust response

Auteurs: Sylvie Dequand
Publié dans: Greener Aviation COnference 2016, 2016
Éditeur: 3AF

Preliminary Design and performance of a morphing winglet for green regional A/C

Auteurs: Ignazio Dimino
Publié dans: Greener Aviation COnference 2016, 2016
Éditeur: 3AF

Research activities of ONERA on laminar wings in the framework of the JTI CLean Sky: transition prediction

Auteurs: Maxime Forte
Publié dans: Greener Aviation COnference 2016, 2016
Éditeur: 3AF

The ASTIB project

Auteurs: Prof. G. Jacazio
Publié dans: 2017
Éditeur: SAE - Society of Automotive Engineers

Experimental shape reconstruction of a morphing wing trailing edge in simulated operative condition

Auteurs: ,F. Amoroso F. Rea, M. Arena, M. C. Noviello R. Pecora, (UNINA) I. Dimino (CIRA)
Publié dans: 2017
Éditeur: ICMAE

Improving Aeroelastic model accuracy and affordability by exploiting wind tunnel test results

Auteurs: M.Di Gifico V.Vaccaro (LDO VEL)
Publié dans: 2017
Éditeur: Department of Aerospace Science and Technology of Politecnico di Milano

Design of aeroelastic wingtip devices for wing load alleviation

Auteurs: F. Toffol F. Fonte Prof S Ricci (POLIMI)
Publié dans: 2017
Éditeur: Department of Aerospace Science and Technology of Politecnico di Milano

Increased Order Aeroservoelastic Modeling in Practice

Auteurs: Reyes M. Climen H Karpel M (CASA)
Publié dans: 2017
Éditeur: Department of Aerospace Science and Technology of Politecnico di Milano

Preliminary Design of the Actuation Mechanism of a Morphing Winglet for Green Regional A/C

Auteurs: I. Dimino, G. Amendola, A. Concilio, G. Andreutti (UNINA) G. Pispola, F. Perni (UMBRA)
Publié dans: 2017
Éditeur: ICAST

Conceptual Design of a Morphing Wingle

Auteurs: G. Amendola, I. Dimino, A. Concilio, G. Andreutti (CIRA) R. Pecora, M. Lo Cascio (UNINA)
Publié dans: 2017
Éditeur: ICMAE

Investigation of a Plasma Synthetic Jet Actuator for Flow Control.

Auteurs: M. Chiatto, L. de Luca (CIRA)
Publié dans: 2017
Éditeur: EFMC11

Numerical and Experimental Frequency Response of Plasma Synthetic Jet Actuator

Auteurs: M. Chiatto, L. de Luca (CIRA)
Publié dans: 2017
Éditeur: AIAA

Influence of Riblets and Laminar Flow Control on the Performance of a Regional Aircraft Configuration

Auteurs: P. Catalano, D. de Rosa (CIRA) Proff. B. Mele, R. Tognaccini, (UNINA) F. Moens (ONERA)
Publié dans: 2017
Éditeur: Prof. M. Quadrio (POLIMI) Prof. P. Luchini (UNISA) Prof. Kwing-So Choi (U-NOT)

Modelling drag reduction devices by slip length at high Reynolds number

Auteurs: Proff. B. Mele, R. Tognaccini (UNINA)
Publié dans: 2017
Éditeur: Prof. M. Quadrio (POLIMI) Prof. P. Luchini (UNISA) Prof. Kwing-So Choi (U-NOT)

Performance characteristics of plasma synthetic jets actuator

Auteurs: M. Chiatto, L. de Luca (CIRA)
Publié dans: 2017
Éditeur: AIMETA

Slip length based boundary condition for modeling drag reduction devices

Auteurs: Proff. B. Mele, R. Tognaccini (UNINA)
Publié dans: 2017
Éditeur: AIAA Aviation 2017

ICAS - 29th Congress of the International Council of the Aeronautical Sciences ADAPTIVE CONTROLLER DESIGN FOR GUST LOAD ALLEVIATION Politecnico di Torino

Auteurs: PoliTO
Publié dans: 2015
Éditeur: ICAS

CS - Structural design of high lift and load control and alleviation devices for a natural laminar flow wing ASAM project PLM

Auteurs: PLM
Publié dans: 2015
Éditeur: PLM

Politecnico di Torino, Italy - 23rd Conference of the Italian Association of Aeronautics and Astronautics LOAD CONTROL AND ALLEVIATION TECHNOLOGY FOR APPLICATION TO FUTURE GREEN REGIONAL AIRCRAFT Politecnico di Torino

Auteurs: PoliTO, FNM VEL
Publié dans: 2015
Éditeur: PoliTO, FNM VEL

Manchester, UK 10th AIAA/CEAS Aeroacoustics Conference, No. AIAA-2004-2955, Manchester, UK, 2004. WENEMOR: Wind Tunnel Tests for the Evaluation of the Installation Effects of Noise Emissions of an Open Rotor Advanced Regional Aircraft

Auteurs: Trinity College Dublin, Pininfarina S.p.A. Italy, Teknosud S.R.L Italy, Univ.Polit. delle Marche Italy, Paragon SA Greece, Eurotech, Italy, FNM VEL
Publié dans: 2015
Éditeur: AIAA/CEAS

Investigation of manufacturing effects by strength assessment, NDI and guided waves based SHM in composite plates reinforced with bonded stringers

Auteurs: Natalino D. Boffa, Ernesto Monaco, Fabrizio Ricci, F. Amoroso
Publié dans: Health Monitoring of Structural and Biological Systems XIII, Numéro PROCEEDINGS VOLUME 10972, 2019, Page(s) 31, ISBN 9781-510626003
Éditeur: SPIE
DOI: 10.1117/12.2516639

Hybrid structural health monitoring on a composite plate manufactured with automatic fibers placement including embedded fiber Bragg gratings and bonded piezoelectric patches

Auteurs: Natalino D. Boffa, Ernesto Monaco, Fabrizio Ricci, Leonardo Lecce, Marco Barile, Vittorio Memmolo
Publié dans: Health Monitoring of Structural and Biological Systems XIII, 2019, Page(s) 27, ISBN 9781-510626003
Éditeur: SPIE
DOI: 10.1117/12.2516537

A SIMULATION METHODOLOGY FOR THE DESIGN OF TRAILING-EDGE FLAP DEPLOYMENT MECHANISM

Auteurs: A. E. ÖNGÜT, E. ALLEGAERT, Y. LEMMENS (SISW)
Publié dans: CAASE18: The Conference on Advancing Analysis & Simulation in Engineering, 2018, Page(s) all pages
Éditeur: CAASE18

Aerodynamic Design, analysis and optimization of an innovative regional aircraft

Auteurs: F. Nicolosi, S. Corcione, P. Della Vecchia, A. De Marco, M. Ruocco, V. Trifari, V. Cusati (UNINA)
Publié dans: ICAS 2018, 2018
Éditeur: ICAS 2018

Real Time Loading Test Rig for Flight Control Actuators Under PHM Experimentation

Auteurs: P. Chiavaroli, A. De Martin, G. Evangelista, G. Jacazio, M. Sorli
Publié dans: Volume 1: Advances in Aerospace Technology, 2018, ISBN 978-0-7918-5200-2
Éditeur: American Society of Mechanical Engineers
DOI: 10.1115/imece2018-86967

Drag reduction of three-dimensional riblets on a at plate turbulent boundary layer

Auteurs: Cafiero, Gioacchino; Iuso, Gaetano (POLITO)
Publié dans: 72nd Annual Meeting of the American Physical Society - Division of Fluid Dynamics, 2019
Éditeur: apsdfd2019

Composite reinforced plates built by co-infusion or secondary bonding techniques: analysis of the effects of manufacturing approach on compression behaviour by mechanical tests, NDI and guided waves based SHM”

Auteurs: Monaco, E., Boffa, N.D., Ricci, F.
Publié dans: AIDAA 2019 Congress, 2019
Éditeur: A.I.D.A.A. – Associazione Italiana di Aeronautica e Astronautica

Flutter analysis of a large civil aircraft in case of free-plays and internal failures of morphing wing flaps mechanical systems

Auteurs: Rosario Pecora, Francesco Amoroso, Ignazio Dimino, Antonio Concilio
Publié dans: Active and Passive Smart Structures and Integrated Systems XIII, 2019, Page(s) 31, ISBN 9781-510625907
Éditeur: SPIE
DOI: 10.1117/12.2514251

"""Morphing wing flaps for large civil transportation aircraft: the evolution of a smart technology across the cleansky program"""

Auteurs: Pecora, R.,
Publié dans: Smart Aircraft Symposium (invited lecture) held at Xi'An Jiaotong University,, 2017
Éditeur: ELSEVIER

Morphing wing flaps for large civil aircraft: the CleanSky-GRA challenge

Auteurs: R. Pecora, F. Amoroso
Publié dans: AIDAA 2019 Congress, 2019
Éditeur: AIDAA

Structural design of a three-modal camber morphing wing flap for large civil aircraft applications

Auteurs: F. Rea, F. Amoroso, R. Pecora,
Publié dans: AIDAA 2019 Congress, 2019
Éditeur: AIDAA

“Aeroelastic stability assessment of a CS-25 category aircraft equipped with morphing wing devices”

Auteurs: M.C. Noviello, F. Amoroso, R. Pecora, I. Dimino, A. Concilio,
Publié dans: AIDAA 2019 Congress, 2019
Éditeur: AIDAA

“ACSIS (Actuation, Control & Sensing Integrated System) for morphing structures”

Auteurs: M. Arena, F. Amoroso, R. Pecora,
Publié dans: AIDAA 2019 Congress, 2019
Éditeur: AIDAA

Aerodynamic Force Breakdown Based on Vortex Force Theory

Auteurs: Linlin Kang, Lorenzo Russo, Renato Tognaccini, Jiezhi Wu, Weidong Su
Publié dans: AIAA Scitech 2019 Forum, 2019, ISBN 978-1-62410-578-4
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-2122

"""High Lift Aerodynamic characteristics of a Three Lifting Surfaces Turboprop Aircraft"""

Auteurs: S. Corcione, P. Della Vecchia, F. Nicolosi, D. Ciliberti and V. Cusati,
Publié dans: AIAA Aviation 2019 Forum, (AIAA 2019-2884),, 2019
Éditeur: AIAA Aviation 2019 FORUM eISBN: 978-1-62410-589-0

“Longitudinal stability issues including propulsive effects on an innovative commercial propeller-driven aircraft”

Auteurs: S. Corcione, P. Della Vecchia, F. Nicolosi, D. Ciliberti and V. Cusati,
Publié dans: AIAA Aviation 2019 Forum, (AIAA 2019-2882), 2019
Éditeur: AIAA Aviation

“Directional stability issues of a three lifting surface aircraft”,

Auteurs: S. Corcione, V. Cusati, F. Nicolosi, D. Ciliberti,
Publié dans: XXV AIDAA Congress, 2019
Éditeur: AIDAA

Slip Length–Based Boundary Condition for Modeling Drag Reduction Devices

Auteurs: Benedetto Mele, Renato Tognaccini
Publié dans: AIAA Journal, Numéro 56/9, 2018, Page(s) 3478-3490, ISSN 0001-1452
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/1.j056589

A Calibrated Lumped Element Model for the Prediction of PSJ Actuator Efficiency Performance

Auteurs: Matteo Chiatto, Andrea Palumbo, Luigi de Luca
Publié dans: Actuators, Numéro 7/1, 2018, Page(s) 10, ISSN 2076-0825
Éditeur: MDPI Multidisciplinary Digital Publishing Institute
DOI: 10.3390/act7010010

Description of Position Control Laws for Functionality Test of a Bi-modal Morphing Flap

Auteurs: Noviello M.C., Rea F., Arena M., Pecora R., Amoroso F.
Publié dans: International Journal of Mechanical Engineering and Robotics Research, 2019, ISSN 2278-0149
Éditeur: IJMERR
DOI: 10.18178/ijmerr.8.1.31-40

Exploitation of a Multifunctional Twistable Wing Trailing-Edge for Performance Improvement of a Turboprop 90-Seats Regional Aircraft

Auteurs: Francesco Rea, Francesco Amoroso, Rosario Pecora, Frederic Moens
Publié dans: Aerospace, Numéro 5/4, 2018, Page(s) 122, ISSN 2226-4310
Éditeur: MDPI Multidisciplinary Digital Publishing Institute
DOI: 10.3390/aerospace5040122

Preliminary Design Process for an Adaptive Winglet

Auteurs: Gianluca Amendola, Ignazio Dimino, Antonio Concilio, Giovanni Andreutti, Rosario Pecora, Marco Lo Cascio
Publié dans: International Journal of Mechanical Engineering and Robotics Research, Numéro 6/6, 2017, Page(s) 83-92, ISSN 2278-0149
Éditeur: IJMERR
DOI: 10.18178/ijmerr.7.1.83-92

Measurements versus Numerical Simulations for Slotted Synthetic Jet Actuator

Auteurs: Andrea Palumbo, Matteo Chiatto, Luigi de Luca
Publié dans: Actuators, Numéro 7/3, 2018, Page(s) 59, ISSN 2076-0825
Éditeur: MDPI Multidisciplinary Digital Publishing Institute
DOI: 10.3390/act7030059

Electro-Actuation System Strategy for a Morphing Flap

Auteurs: Maurizio Arena, Francesco Amoroso, Rosario Pecora, Salvatore Ameduri
Publié dans: Aerospace, Numéro 6/1, 2019, Page(s) 1, ISSN 2226-4310
Éditeur: MDPI Multidisciplinary Digital Publishing Institute
DOI: 10.3390/aerospace6010001

Plasma Synthetic Jet Actuators for Active Flow Control

Auteurs: Haohua Zong, Matteo Chiatto, Marios Kotsonis, Luigi de Luca
Publié dans: Actuators, Numéro 7/4, 2018, Page(s) 77, ISSN 2076-0825
Éditeur: MDPI Multidisciplinary Digital Publishing Institute
DOI: 10.3390/act7040077

Numerical and experimental validation of a full scale servo-actuated morphing aileron model

Auteurs: Maurizio Arena, Francesco Amoroso, Rosario Pecora, Gianluca Amendola, Ignazio Dimino, Antonio Concilio
Publié dans: Smart Materials and Structures, Numéro 27/10, 2018, Page(s) 105034, ISSN 0964-1726
Éditeur: Institute of Physics Publishing
DOI: 10.1088/1361-665x/aad7d9

Numerical and experimental characterization of a double-orifice synthetic jet actuator

Auteurs: Matteo Chiatto, Francesco Capuano, Luigi de Luca
Publié dans: Meccanica, Numéro 53/11-12, 2018, Page(s) 2883-2896, ISSN 0025-6455
Éditeur: Kluwer Academic Publishers
DOI: 10.1007/s11012-018-0866-7

Application of laser Doppler vibrometry for ultrasonic velocity assessment in a composite panel with defect

Auteurs: L. Maio, F. Ricci, V. Memmolo, E. Monaco, N.D. Boffa
Publié dans: Composite Structures, Numéro 184, 2018, Page(s) 1030-1039, ISSN 0263-8223
Éditeur: Elsevier BV
DOI: 10.1016/j.compstruct.2017.10.059

Preliminary acousto-ultrasonic investigation for multi-parameter transducer self-diagnostic system in composites

Auteurs: V. Memmolo, Y.J. Park, M. Lilov, E. Monaco, F. Ricci
Publié dans: Composite Structures, Numéro 202, 2018, Page(s) 1229-1238, ISSN 0263-8223
Éditeur: Elsevier BV
DOI: 10.1016/j.compstruct.2018.05.125

Aero-servo-elastic design of a morphing wing trailing edge system for enhanced cruise performance

Auteurs: Maurizio Arena, Antonio Concilio, Rosario Pecora
Publié dans: Aerospace Science and Technology, Numéro 86, 2019, Page(s) 215-235, ISSN 1270-9638
Éditeur: Elsevier BV
DOI: 10.1016/j.ast.2019.01.020

Guided wave propagation and scattering for structural health monitoring of stiffened composites

Auteurs: V. Memmolo, E. Monaco, N.D. Boffa, L. Maio, F. Ricci
Publié dans: Composite Structures, Numéro 184, 2018, Page(s) 568-580, ISSN 0263-8223
Éditeur: Elsevier BV
DOI: 10.1016/j.compstruct.2017.09.067

Flutter Clearance Investigation of Camber-Morphing Aileron Tailored for a Regional Aircraft

Auteurs: Maurizio Arena, Rita Palumbo, Rosario Pecora, Francesco Amoroso, Gianluca Amendola, Ignazio Dimino
Publié dans: Journal of Aerospace Engineering, Numéro 32/2, 2019, Page(s) 04018146, ISSN 0893-1321
Éditeur: American Society of Civil Engineers
DOI: 10.1061/(asce)as.1943-5525.0000973

Design of a PHM system for electro-mechanical flight controls: a roadmap from preliminary analyses to iron-bird validation

Auteurs: Andrea De Martin, Giovanni Jacazio, Massimo Sorli
Publié dans: MATEC Web of Conferences, Numéro 304, 2019, Page(s) 04018, ISSN 2261-236X
Éditeur: EDP sciences
DOI: 10.1051/matecconf/201930404018

Lumped parameters modelling of the EMAs’ ball screw drive with special consideration to ball/grooves interactions to support model-based health monitoring

Auteurs: Antonio Carlo Bertolino, Massimo Sorli, Giovanni Jacazio, Stefano Mauro
Publié dans: Mechanism and Machine Theory, Numéro 137, 2019, Page(s) 188-210, ISSN 0094-114X
Éditeur: Pergamon Press Ltd.
DOI: 10.1016/j.mechmachtheory.2019.03.022

Prediction of the acoustic shielding by aircraft empennage for contra-rotating open rotors

Auteurs: L Sanders, D-C Mincu, PL Vitagliano, M Minervino, J Kennedy, G Bennett
Publié dans: International Journal of Aeroacoustics, Numéro 16/7-8, 2017, Page(s) 626-648, ISSN 1475-472X
Éditeur: Multi-Science Publishing Co. Ltd
DOI: 10.1177/1475472x17734334

Aerodynamic Shape Design and Validation of an Advanced High-Lift Device for a Regional Aircraft with Morphing Droop Nose

Auteurs: Alessandro De Gaspari, Frédéric Moens
Publié dans: International Journal of Aerospace Engineering, Numéro 2019, 2019, Page(s) 1-21, ISSN 1687-5966
Éditeur: Hindawi Publishing Corporation
DOI: 10.1155/2019/7982168

Powered wind tunnel tests setup of the IRON innovative turboprop aircraft

Auteurs: Danilo Ciliberti, Vincenzo Cusati, Pierluigi Della Vecchia, Salvatore Corcione, Fabrizio Nicolosi
Publié dans: MATEC Web of Conferences, Numéro 304, 2019, Page(s) 02022, ISSN 2261-236X
Éditeur: MATEC
DOI: 10.1051/matecconf/201930402022

Feasibility study of innovative regional turboprop: an overview of the European project IRON

Auteurs: Salvatore Corcione, Vittorio Trifari, Fabrizio Nicolosi, Vincenzo Cusati, Danilo Ciliberti, Pierluigi Della Vecchia
Publié dans: MATEC Web of Conferences, Numéro 304, 2019, Page(s) 03014, ISSN 2261-236X
Éditeur: MATEC
DOI: 10.1051/matecconf/201930403014

Understanding of structural and acoustic behaviour of stiffened composite panels for fuselage applications FNM VEL

Auteurs: FNM VEL
Publié dans: 2015
Éditeur: FNM VEL

"""CS - Composite Fuselage One Piece Barrel (OPB): Integrated Development and Prototype Demonstration AFLOG project OMI"""

Auteurs: OMI
Publié dans: 2015
Éditeur: OMI

Optical fibres and piezoelectric technologies applications in flight and ground demonstrations. Fraunhofer

Auteurs: Fraunhofer
Publié dans: 2015
Éditeur: Fraunhofer

Composite Platform SHM design from flight and ground demonstration requirements

Auteurs: FNM VEL
Publié dans: 2015
Éditeur: FNM VEL

"""CS - Design Considerations of an Autonomous Wireless Sensor Network for Structural Health Monitoring in Aircraft WILDCRAFT project CEIT """

Auteurs: CEIT
Publié dans: 2015
Éditeur: CEIT

Structural Health Monitoring of a composite stiffened panel FNM VEL

Auteurs: FNM VEL
Publié dans: 2015
Éditeur: FNM VEL

CS - Airframe Noise Reduction Technologies applied to High-Lift Devices of Future Green Regional Aircraft CIRA

Auteurs: cira
Publié dans: 2015
Éditeur: CIRA

Full-scale Wind Tunnel Demonstration of Nose Landing Gear Low-Noise Technologies for Future Regional Aircraft “ALLEGRA” project Trinity College Dublin

Auteurs: Trinity College Dublin
Publié dans: 2015
Éditeur: Trinity College Dublin

Brussels - Clean Sky General Forum - CS - Airframe Noise Reduction Technologies applied to High-Lift Devices of Future Green Regional Aircraft CIRA

Auteurs: CIRA
Publié dans: 2015
Éditeur: CIRA

CS - ETRIOLLA Actuation and measurement technologies for WTT of the innovative regional transonic wing ETRIOLLA project IBK Innovation GmbH

Auteurs: IBK
Publié dans: 2015
Éditeur: IBK

London - Droop Nose Technology toward Future Green Regional Aircraft: Development and Prototype Demonstration Fraunhofer

Auteurs: Fraunhofer
Publié dans: 2015
Éditeur: Fraunhofer

Design, development and manufacturing of an electro-mechanical actuator and test rig for AiRcrafts Main LandIng Gear AcTuation systems ARMLIGhT project CESA Spain

Auteurs: CESA
Publié dans: 2015
Éditeur: CESA

Airframe Noise Reduction Technologies applied to High-Lift Devices of Future Green Regional Aircraft CIRA, Italy, INCAS, Romania, FOI, Chalmers University of technology, Sweden and ONERA, France

Auteurs: CIRA, INCAS, FOI, Chalmers University of technology, ONERA
Publié dans: 2015
Éditeur: CIRA, INCAS, FOI, Chalmers University of technology, ONERA

CS - ADAVES advanced avionics equipment simulation ADAVES project

Auteurs: EDISOFT-EMPRESA DE SERVICOS E DESENVOLVIMENTO DE SOFTWARE SA
Publié dans: 2015
Éditeur: EDISOFT-EMPRESA DE SERVICOS E DESENVOLVIMENTO DE SOFTWARE SA

An Electrical POwer Center for Aeronautical Loads “EPOCAL” project Seconda Università degli Studi di Napoli

Auteurs: Seconda Università degli studi di Napoli
Publié dans: 2015
Éditeur: Seconda Università degli studi di Napoli

Future Green Regional A/C Gust Load Alleviation control system experimental validation through innovative WT tests GLAMOUR project Politecnico di Milano

Auteurs: Politecnico di Milano
Publié dans: 2014, 2015
Éditeur: Politecnico di Milano

Future Green Regional A/C Transonic Laminar Wing experimental assessment Through innovative WT tests Drag passive reduction by riblets technology: Results from GRA ITD studies and prospects for further achievements Università di Napoli, Politecnico di Torino

Auteurs: "Università di Napoli ""Federico II"", Politecnico di Torino"
Publié dans: 2015
Éditeur: "Università di Napoli ""Federico II"", Politecnico di Torino"

"""Future Green Regional A/C Transonic Laminar Wing experimental assessment through innovative WT tests ETRIOLLA project IBK """

Auteurs: IBK
Publié dans: 2015
Éditeur: IBK

Aerodynamic Design Based on Numerical Optimization of a Green ATF Regional Aircraft Piaggio Aerospace, FNM VEL

Auteurs: Piaggio Aerospace, FNM VEL
Publié dans: 2015
Éditeur: Piaggio Aerospace, FNM VEL

Future Green Regional A/C Transonic Laminar Wing experimental assessment through innovative WT tests Landing Gear Aiframe Noise Reduction Technology Development for Future Green Regional Aircraft CIRA

Auteurs: CIRA
Publié dans: 2015
Éditeur: CIRA

Optimization of Morphing Wings for Improved Environmental Performance MAWS project University of Bristol

Auteurs: University of Bristol
Publié dans: 2014, 2015
Éditeur: University of Bristol

Future Green Regional A/C Transonic Laminar Wing experimental assessment through innovative WT tests Wind Tunnel Test and CFD/CAA Analysis on a Scaled Model of a Nose Landing Gear Fraunhofer

Auteurs: Fraunhofer
Publié dans: 2014, 2015
Éditeur: Fraunhofer

Natural Laminar Flow Transonic Wing Design applied to Future Innovative Green Regional Aircraft

Auteurs: ONERA, FNM VEL, CIRA
Publié dans: 2015
Éditeur: ONERA, FNM VEL, CIRA

Future Green Regional A/C Transonic Laminar Wing experimental assessment through innovative WT tests Load Control and Alleviation Technology for application to future Green Regional Aircr aft FNM VEL

Auteurs: FNM VEL
Publié dans: 2014, 2015
Éditeur: FNM VEL

Innovative Electrical Energy Management strategy for Future Regional All-Electric Aircraft FNM VEL

Auteurs: FNM VEL
Publié dans: 2015
Éditeur: FNM VEL

Future Green Regional A/C Transonic Laminar Wing experimental assessment through innovative WT tests Design, Development and Test of Synthetic Jets Actuators for Future Green Regional Aircraft Fraunhofer

Auteurs: Fraunhofer
Publié dans: 2015
Éditeur: Fraunhofer

Future Green Regional A/C Transonic Laminar Wing experimental assessment through innovative WT tests Smart Droop Nose for application to Laminar Wing of future Green Regional A/C Fraunhofer

Auteurs: Fraunhofer
Publié dans: 2015
Éditeur: Fraunhofer

ATR : Green FMS functions for a green Aircraft

Auteurs: Thales Avionics, ATR
Publié dans: 2015
Éditeur: Thales Avionics, ATR

Future Green Regional A/C Transonic Laminar Wing experimental assessment through innovative WT tests Aiframe Noise Reduction Technologies applied to High-Lift Devices of Future Green Regional Aircraft CIRA

Auteurs: CIRA
Publié dans: 2015
Éditeur: CIRA

A SIMULATION METHODOLOGY FOR THE DESIGN OF TRAILING-EDGE FLAP DEPLOYMENT MECHANISM

Auteurs: A. E. ÖNGÜT, E. ALLEGAERT, Y. LEMMENS (SISW)
Publié dans: CAASE18, The Conference on Advancing Analysis & Simulation in Engineering, 2018
Éditeur: CAASE18

Comprehensive Robust Adaptive Controller for Gust Load Alleviation

Auteurs: Elisa Capello,* Giorgio Guglieri, and Fulvia Quagliotti
Publié dans: THE SCIENTIFIC WORLD JOURNAL, 2015, ISSN 1537-744X
Éditeur: ScientificWorld, Inc.

Droits de propriété intellectuelle

METHODS OF MANUFACTURING PANELS OF COMPOSITE MATERIAL REINFORCED WITH CLOSED-SECTION STRINGERS

Numéro de demande/publication: 16 177404
Date: 2016-07-01
Demandeur(s): LEONARDO - SOCIETA PER AZIONI

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