Overall Preliminary Sizing and Optimization of the Metallic Structures of a PrandtlPlane Civil Transport Aircraft The paper aims at presenting and summarizing the activities carried out on the structural aspects of a box-wing aircraft, called PrandtlPlane, proposed as a more efficient alternative to present commercial aircraft. The results hereby shown represent the major achievements in […]
Conferences
PARSIFAL project: interim results presented at AIAA Aviation Forum 2018 (Atlanta, USA)
Conceptual design of a box-wing aircraft for the air transport of the future The paper aims to present the conceptual design of a box-wing aircraft, called PrandtlPlane, proposed as an efficient alternative for future air transport. Activities and results described here are part of a research project called PARSIFAL (“Prandtlplane ARchitecture for the Sustainable Improvement […]
A new paper published in Transportation Research Procedia (Elsevier): “Preliminary transonic CFD analyses of a PrandtlPlane transport aircraft” (Open Access)
In the framework of the PARSIFAL research project, funded by the European Community in the Horizon 2020 program, the PrandtlPlane (PrP) configuration has been proposed as an innovative alternative to the current commercial aircraft of conventional architecture; the PrP configuration development is presented in order to satisfy the future air traffic growing requirements with better […]
A new paper published in Aerotecnica Missili & Spazio (Springer): “PARSIFAL Project: a Breakthrough Innovation in Air Transport”
PARSIFAL is a Horizon 2020 project, started on May 2017, with the aim to design an innovative aircraft, based on the “PrandtlPlane” (PrP) configuration, for the civil aviation of the future. The PrP configuration allows us to reduce the fuel consumption and the external noise, especially during low speed flight. The high aerodynamic performances are […]
HYPSTAIR results published in the proceedings of the “Variational Analysis and Aerospace Engineering” Workshop (Erice, Sept. 2015)
HyPSim: A Simulation Tool for Hybrid Aircraft Performance Analysis This work presents performance prediction contribution provided by the research team at the University of Pisa. The results are part of the HYPSTAIR (Development and validation of hybrid propulsion system components and sub-systems for electrical aircraft) European project on the development and validation of hybrid propulsion […]