Regional Aircraft

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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