Prandtlplane ARchitecture for the Sustainable Improvement of Future AirpLanes

Risultati finali

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.

Pubblicazioni

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

Autori: K. Abu Salem, G. Palaia, V. Cipolla, V. Binante
Pubblicato in: AIDAA 2019 Conference Proceedings, 2019
Editore: Italian Association of Aeronautics and Astronautics

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

Autori: C. Varriale, A.Raju Kulkarni1, G. La Rocca, M. Voskuijl
Pubblicato in: AIDAA 2019 Conference Proceedings, 2019
Editore: Italian Association of Aeronautics and Astronautics

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

Autori: Carini, Marco; Méheut, Michaël; Sanders, Laurent
Pubblicato in: AIDAA 2019 Conference Proceedings, 2019
Editore: Associazione Italiana di Aeronautica e Astronautica (AIDAA)

Aerodynamic design and preliminary optimization of a commercial PrandtlPlane aircraft

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

Comparative Design and Sensitivity studies on box-wing airplanes

Autori: R.J.M. Elmendorp, G. La Rocca
Pubblicato in: AIDAA 2019 Conference Proceedings, 2019
Editore: Italian Association of Aeronautics and Astronautics

On the preliminary design of PrandtlPlane civil transport aircraft

Autori: Frediani Aldo, Vittorio Cipolla, Karim Abu Salem, Marco Picchi Scardaoni
Pubblicato in: EUCASS 2017 Conference Proceedigns, 2017
Editore: 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

Autori: Vittorio Cipolla, Aldo Frediani, Karim Abu Salem, Marco Picchi Scardaoni, Alessio Nuti, Vincenzo Binante
Pubblicato in: 2018 Aviation Technology, Integration, and Operations Conference, 2018, ISBN 978-1-62410-556-2
Editore: 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

Autori: PICCHI SCARDAONI, MARCO CIPOLLA, VITTORIO BINANTE, VINCENZO
Pubblicato in: EUCASS 2019, 2019
Editore: EUCASS
DOI: 10.13009/eucass2019-802

Trim for Maximum Control Authority using the Attainable Moment Set

Autori: Carmine Varriale, Mark Voskuijl, Leo L. Veldhuis
Pubblicato in: AIAA Scitech 2020 Forum, 2020, ISBN 978-1-62410-595-1
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-1265

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

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

Aerodynamic analysis and optimization of a boxwing architecture for commercial airplanes

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

Preliminary Take-Off Analysis and Simulation of PrandtlPlane Commercial Aircraft

Autori: K. Abu Salem, G. Palaia, M. Bianchi, D. Zanetti, V. Cipolla, V. Binante
Pubblicato in: Aerotecnica Missili & Spazio, Numero 99/3, 2020, Pagina/e 203-216, ISSN 2524-6968
Editore: Springer Nature
DOI: 10.1007/s42496-020-00056-0

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

Autori: Marco Picchi Scardaoni, Marco Montemurro
Pubblicato in: Structural and Multidisciplinary Optimization, 2020, ISSN 1615-147X
Editore: Springer Verlag
DOI: 10.1007/s00158-020-02586-4

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

Autori: Michele I Izzi, Marco Montemurro, Anita Catapano, Daniele Fanteria, Jérôme Pailhès
Pubblicato in: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020, Pagina/e 095441002093933, ISSN 0954-4100
Editore: Mechanical Engineering Publications Ltd.
DOI: 10.1177/0954410020939338

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

Autori: Marco Picchi Scardaoni, Marco Montemurro, Enrico Panettieri
Pubblicato in: Aerospace Science and Technology, Numero 106, 2020, Pagina/e 106156, ISSN 1270-9638
Editore: Elsevier BV
DOI: 10.1016/j.ast.2020.106156

Blending constraints for composite laminates in polar parameters space

Autori: Enrico Panettieri, Marco Montemurro, Anita Catapano
Pubblicato in: Composites Part B: Engineering, Numero 168, 2019, Pagina/e 448-457, ISSN 1359-8368
Editore: 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

Autori: Enrico Panettieri, Marco Montemurro, Daniele Fanteria, Francesco Coccia
Pubblicato in: Journal of Optimization Theory and Applications, 2020, ISSN 0022-3239
Editore: 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

Autori: Marco Picchi Scardaoni, Marco Montemurro, Enrico Panettieri, Anita Catapano
Pubblicato in: Structural and Multidisciplinary Optimization, 2020, ISSN 1615-147X
Editore: Springer Verlag
DOI: 10.1007/s00158-020-02725-x

Preliminary stability analysis methods for PrandtlPlane aircraft in subsonic conditions

Autori: Vittorio Cipolla, Karim Abu Salem, Filippo Bachi
Pubblicato in: Aircraft Engineering and Aerospace Technology, Numero 91/3, 2019, Pagina/e 525-537, ISSN 1748-8842
Editore: 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

Autori: Sam de de Wringer, Carmine Varriale, Fabrizio Oliviero
Pubblicato in: Aerospace, Numero 7/9, 2020, Pagina/e 134, ISSN 2226-4310
Editore: MDPI
DOI: 10.3390/aerospace7090134

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

Autori: A. Frediani, V. Cipolla, V. Binante, K. Abu Salem, M. Maganzi
Pubblicato in: Aerotecnica, Missili & Spazio, Numero Vol. 96, N. 3, 2017, Pagina/e 136-147, ISSN 0365-7442
Editore: Italian Association of Aeronautics and Astronautics (AIDAA)
DOI: 10.19249/ams.v96i3.311

Preliminary transonic CFD analyses of a PrandtlPlane transport aircraft

Autori: Cipolla Vittorio, Frediani Aldo, Abu Salem Karim, Binante Vincenzo, Rizzo Emanuele, Maganzi Marco
Pubblicato in: Transportation Research Procedia, Numero 29, 2018, Pagina/e 82-91, ISSN 2352-1465
Editore: 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

Autori: Alessio Nuti, Francesco Bertini, Vittorio Cipolla, Gianpietro Di Rito
Pubblicato in: Aerotecnica Missili & Spazio, Numero Vol. 97, N. 2, 2018, Pagina/e 85-95, ISSN 0365-7442
Editore: Italian Association of Aeronautics and Astronautics (AIDAA)
DOI: 10.19249/ams.v97i2.341

PARSIFAL Project: a breakthrough innovation in air transport

Autori: Karim Abu Salem, Vincenzo Binante, Vittorio Cipolla, Marco Maganzi
Pubblicato in: Aerotecnica, Missili & Spazio, Numero Vol. 97, N. 1, 2018, Pagina/e 40-46, ISSN 0365-7442
Editore: Italian Association of Aeronautics and Astronautics (AIDAA)
DOI: 10.19249/ams.v97i1.337

Conceptual design of PrandtlPlane civil transport aircraft

Autori: A Frediani, Vittorio Cipolla, K Abu Salem, V Binante, M Picchi Scardaoni
Pubblicato in: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, Pagina/e 095441001982643, ISSN 0954-4100
Editore: 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

Autori: Marco Picchi Scardaoni, Aldo Frediani
Pubblicato in: Aerotecnica Missili & Spazio, Numero 98/1, 2019, Pagina/e 45-61, ISSN 0365-7442
Editore: AIDAA
DOI: 10.1007/s42496-018-00004-z

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

Autori: Michele Iacopo Izzi, Marco Montemurro, Anita Catapano, Jérôme Pailhès
Pubblicato in: Composite Structures, Numero 237, 2020, Pagina/e 111908, ISSN 0263-8223
Editore: 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

Autori: G.A. Fiordilino, M.I. Izzi, M. Montemurro
Pubblicato in: Mechanics of Materials, 2020, Pagina/e 103574, ISSN 0167-6636
Editore: Elsevier BV
DOI: 10.1016/j.mechmat.2020.103574

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

Autori: Marco Picchi Scardaoni, Marco Montemurro
Pubblicato in: European Journal of Mechanics - A/Solids, 2020, Pagina/e 104112, ISSN 0997-7538
Editore: Elsevier BV
DOI: 10.1016/j.euromechsol.2020.104112

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

Autori: Vittorio Cipolla, Aldo Frediani, Karim Abu Salem, Marco Picchi Scardaoni, Vincenzo Binante
Pubblicato in: MATEC Web of Conferences, Numero 304, 2019, Pagina/e 01024, ISSN 2261-236X
Editore: MATEC
DOI: 10.1051/matecconf/201930401024

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