Prandtlplane ARchitecture for the Sustainable Improvement of Future AirpLanes

Livrables

Report on operational and economic assessment

Analysis of the economic and logistics impact for transport operators (This document is accessible to Advisory Board members too.)

Advanced flight control concepts for the PrandtlPlane to increase safety and passenger comfort

Exploration of the potential for advanced flight control concepts (e.g.: direct lift control and direct side-force control) and evaluation of possible expansion of the flight envelope

Aircraft performance analysis and mission profile optimization

Definition of optimum mission profiles for PrPs whilst taking into account actual constraints (air traffic control, block time, etc.)

Report on socio-economic scenarios and expectations

Forecasting of air passenger demand for identifying the relevant and deriving future demand prognostics (This document is accessible to Advisory Board members too)

Preliminary design of the reference PrandtlPlane

Conceptual design of the PrP configuration, including a preliminary analysis of system integration

Requirements for the adoption of the PrandtlPlane as mean of transport

Definition of Top Level Aircraft Requirements according to the identified reference Air Transport System (This document is accessible to Advisory Board members too)

Aerodynamic and acoustic analysis of the baseline PrandtlPlane

Aerodynamic analysis of the reference PrP in cruise, low-speed conditions (including acoustics), longitudinal stability and control surface effectiveness.

Feasibility study on the use of very large bypass ratio turbofan engines for the PrandtlPlane

Feasibility study on the use of very large bypass ratio turbofan engines for the PrandtlPlane (TUD, M30)

PrandtlPlane performance analysis and scaling procedures

Performance analysis from both Aircraft and the Air Transport System perspectives and definition of criteria for the performance prediction the of different size PrP

Project Website

Project website which will be used both for dissemination purposes and to provide partners with any time access to project documents. This will be made possible including a reserved area to the area.

Publications

PRELIMINARY TAKE-OFF ANALYSIS AND SIMULATION FOR A PRANDTLPLANE COMMERCIAL AIRCRAFT

Auteurs: K. Abu Salem, G. Palaia, V. Cipolla, V. Binante
Publié dans: AIDAA 2019 Conference Proceedings, 2019
Éditeur: Italian Association of Aeronautics and Astronautics

A Hybrid, configuration-agnostic approach to aircraft control surface sizing

Auteurs: C. Varriale, A.Raju Kulkarni1, G. La Rocca, M. Voskuijl
Publié dans: AIDAA 2019 Conference Proceedings, 2019
Éditeur: Italian Association of Aeronautics and Astronautics

Aerodynamic and Acoustic analysis of a preliminary PrandtlPlane configuration within the framework of the PARSIFAL project

Auteurs: Carini, Marco; Méheut, Michaël; Sanders, Laurent
Publié dans: AIDAA 2019 Conference Proceedings, 2019
Éditeur: Associazione Italiana di Aeronautica e Astronautica (AIDAA)

Aerodynamic design and preliminary optimization of a commercial PrandtlPlane aircraft

Auteurs: ABU SALEM, Karim; CIPOLLA, Vittorio; CARINI, Marco; MEHEUT, Michael; KANELLOPOULOS, Stylianos; BINANTE, Vincenzo; MAGANZI, Marco
Publié dans: EUCASS 2019 Conference Proceedings, 2019
Éditeur: EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
DOI: 10.13009/EUCASS2019-741

Comparative Design and Sensitivity studies on box-wing airplanes

Auteurs: R.J.M. Elmendorp, G. La Rocca
Publié dans: AIDAA 2019 Conference Proceedings, 2019
Éditeur: Italian Association of Aeronautics and Astronautics

On the preliminary design of PrandtlPlane civil transport aircraft

Auteurs: Frediani Aldo, Vittorio Cipolla, Karim Abu Salem, Marco Picchi Scardaoni
Publié dans: EUCASS 2017 Conference Proceedigns, 2017
Éditeur: European Conference for AeroSpace Sciences (EUCASS)
DOI: 10.13009/EUCASS2017-546

Conceptual design of a box-wing aircraft for the air transport of the future

Auteurs: Vittorio Cipolla, Aldo Frediani, Karim Abu Salem, Marco Picchi Scardaoni, Alessio Nuti, Vincenzo Binante
Publié dans: 2018 Aviation Technology, Integration, and Operations Conference, 2018, ISBN 978-1-62410-556-2
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2018-3660

Overall Preliminary Sizing and Optimization of the Metallic Structures of a PrandtlPlane Civil Transport Aircraft

Auteurs: PICCHI SCARDAONI, MARCO CIPOLLA, VITTORIO BINANTE, VINCENZO
Publié dans: EUCASS 2019, 2019
Éditeur: EUCASS
DOI: 10.13009/eucass2019-802

Trim for Maximum Control Authority using the Attainable Moment Set

Auteurs: Carmine Varriale, Mark Voskuijl, Leo L. Veldhuis
Publié dans: AIAA Scitech 2020 Forum, 2020, ISBN 978-1-62410-595-1
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-1265

Preliminary design and performance analysis of a box-wing transport aircraft

Auteurs: Vittorio Cipolla, Karim Abu Salem, Marco Picchi Scardaoni, Vincenzo Binante
Publié dans: AIAA Scitech 2020 Forum, 2020, ISBN 978-1-62410-595-1
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-0267

Aerodynamic analysis and optimization of a boxwing architecture for commercial airplanes

Auteurs: Marco Carini, Michael Meheut, Stylianos Kanellopoulos, Vittorio Cipolla, Karim Abu Salem
Publié dans: AIAA Scitech 2020 Forum, 2020, ISBN 978-1-62410-595-1
Éditeur: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-1285

Preliminary Take-Off Analysis and Simulation of PrandtlPlane Commercial Aircraft

Auteurs: K. Abu Salem, G. Palaia, M. Bianchi, D. Zanetti, V. Cipolla, V. Binante
Publié dans: Aerotecnica Missili & Spazio, Numéro 99/3, 2020, Page(s) 203-216, ISSN 2524-6968
Éditeur: Springer Nature
DOI: 10.1007/s42496-020-00056-0

A general global-local modelling framework for the deterministic optimisation of composite structures

Auteurs: Marco Picchi Scardaoni, Marco Montemurro
Publié dans: Structural and Multidisciplinary Optimization, 2020, ISSN 1615-147X
Éditeur: Springer Verlag
DOI: 10.1007/s00158-020-02586-4

Multi-scale optimisation of thin-walled structures by considering a global/local modelling approach

Auteurs: Michele I Izzi, Marco Montemurro, Anita Catapano, Daniele Fanteria, Jérôme Pailhès
Publié dans: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020, Page(s) 095441002093933, ISSN 0954-4100
Éditeur: Mechanical Engineering Publications Ltd.
DOI: 10.1177/0954410020939338

PrandtlPlane wing-box least-weight design: A multi-scale optimisation approach

Auteurs: Marco Picchi Scardaoni, Marco Montemurro, Enrico Panettieri
Publié dans: Aerospace Science and Technology, Numéro 106, 2020, Page(s) 106156, ISSN 1270-9638
Éditeur: Elsevier BV
DOI: 10.1016/j.ast.2020.106156

Blending constraints for composite laminates in polar parameters space

Auteurs: Enrico Panettieri, Marco Montemurro, Anita Catapano
Publié dans: Composites Part B: Engineering, Numéro 168, 2019, Page(s) 448-457, ISSN 1359-8368
Éditeur: Pergamon Press Ltd.
DOI: 10.1016/j.compositesb.2019.03.040

Multi-scale Least-Weight Design of a Wing-Box Through a Global/Local Modelling Approach

Auteurs: Enrico Panettieri, Marco Montemurro, Daniele Fanteria, Francesco Coccia
Publié dans: Journal of Optimization Theory and Applications, 2020, ISSN 0022-3239
Éditeur: Kluwer Academic/Plenum Publishers
DOI: 10.1007/s10957-020-01693-y

New blending constraints and a stack-recovery strategy for the multi-scale design of composite laminates

Auteurs: Marco Picchi Scardaoni, Marco Montemurro, Enrico Panettieri, Anita Catapano
Publié dans: Structural and Multidisciplinary Optimization, 2020, ISSN 1615-147X
Éditeur: Springer Verlag
DOI: 10.1007/s00158-020-02725-x

Preliminary stability analysis methods for PrandtlPlane aircraft in subsonic conditions

Auteurs: Vittorio Cipolla, Karim Abu Salem, Filippo Bachi
Publié dans: Aircraft Engineering and Aerospace Technology, Numéro 91/3, 2019, Page(s) 525-537, ISSN 1748-8842
Éditeur: Emerald Group Publishing Ltd.
DOI: 10.1108/AEAT-12-2017-0284

A Generalized Approach to Operational, Globally Optimal Aircraft Mission Performance Evaluation, with Application to Direct Lift Control

Auteurs: Sam de de Wringer, Carmine Varriale, Fabrizio Oliviero
Publié dans: Aerospace, Numéro 7/9, 2020, Page(s) 134, ISSN 2226-4310
Éditeur: MDPI
DOI: 10.3390/aerospace7090134

WAGNER: a new code for parametrical structural study of fuselages of civil transport aircraft

Auteurs: A. Frediani, V. Cipolla, V. Binante, K. Abu Salem, M. Maganzi
Publié dans: Aerotecnica, Missili & Spazio, Numéro Vol. 96, N. 3, 2017, Page(s) 136-147, ISSN 0365-7442
Éditeur: Italian Association of Aeronautics and Astronautics (AIDAA)
DOI: 10.19249/ams.v96i3.311

Preliminary transonic CFD analyses of a PrandtlPlane transport aircraft

Auteurs: Cipolla Vittorio, Frediani Aldo, Abu Salem Karim, Binante Vincenzo, Rizzo Emanuele, Maganzi Marco
Publié dans: Transportation Research Procedia, Numéro 29, 2018, Page(s) 82-91, ISSN 2352-1465
Éditeur: Elsevier B.V.
DOI: 10.1016/j.trpro.2018.02.008

Design of a Fuselage-Mounted Main Landing Gear of a Medium-Size Civil Transport Aircraft

Auteurs: Alessio Nuti, Francesco Bertini, Vittorio Cipolla, Gianpietro Di Rito
Publié dans: Aerotecnica Missili & Spazio, Numéro Vol. 97, N. 2, 2018, Page(s) 85-95, ISSN 0365-7442
Éditeur: Italian Association of Aeronautics and Astronautics (AIDAA)
DOI: 10.19249/ams.v97i2.341

PARSIFAL Project: a breakthrough innovation in air transport

Auteurs: Karim Abu Salem, Vincenzo Binante, Vittorio Cipolla, Marco Maganzi
Publié dans: Aerotecnica, Missili & Spazio, Numéro Vol. 97, N. 1, 2018, Page(s) 40-46, ISSN 0365-7442
Éditeur: Italian Association of Aeronautics and Astronautics (AIDAA)
DOI: 10.19249/ams.v97i1.337

Conceptual design of PrandtlPlane civil transport aircraft

Auteurs: A Frediani, Vittorio Cipolla, K Abu Salem, V Binante, M Picchi Scardaoni
Publié dans: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, Page(s) 095441001982643, ISSN 0954-4100
Éditeur: Mechanical Engineering Publications Ltd.
DOI: 10.1177/0954410019826435

Analytical and Finite Element Approach for the In-plane Study of Frames of Non-conventional Civil Aircraft

Auteurs: Marco Picchi Scardaoni, Aldo Frediani
Publié dans: Aerotecnica Missili & Spazio, Numéro 98/1, 2019, Page(s) 45-61, ISSN 0365-7442
Éditeur: AIDAA
DOI: 10.1007/s42496-018-00004-z

A multi-scale two-level optimisation strategy integrating a global/local modelling approach for composite structures

Auteurs: Michele Iacopo Izzi, Marco Montemurro, Anita Catapano, Jérôme Pailhès
Publié dans: Composite Structures, Numéro 237, 2020, Page(s) 111908, ISSN 0263-8223
Éditeur: Elsevier BV
DOI: 10.1016/j.compstruct.2020.111908

A general isogeometric polar approach for the optimisation of variable stiffness composites: Application to eigenvalue buckling problems

Auteurs: G.A. Fiordilino, M.I. Izzi, M. Montemurro
Publié dans: Mechanics of Materials, 2020, Page(s) 103574, ISSN 0167-6636
Éditeur: Elsevier BV
DOI: 10.1016/j.mechmat.2020.103574

Convex or non-convex? On the nature of the feasible domain of laminates

Auteurs: Marco Picchi Scardaoni, Marco Montemurro
Publié dans: European Journal of Mechanics - A/Solids, 2020, Page(s) 104112, ISSN 0997-7538
Éditeur: Elsevier BV
DOI: 10.1016/j.euromechsol.2020.104112

The Project “Parsifal”: Prandtlplane Architecture For The Sustainable Improvement Of Future Airplanes

Auteurs: Vittorio Cipolla, Aldo Frediani, Karim Abu Salem, Marco Picchi Scardaoni, Vincenzo Binante
Publié dans: MATEC Web of Conferences, Numéro 304, 2019, Page(s) 01024, ISSN 2261-236X
Éditeur: MATEC
DOI: 10.1051/matecconf/201930401024

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