Box-wing architecture and hybrid-electric propulsion for regional aircraft: paper presented at EUCASS-3AF 2022 Conference (Lille, FR) available on-line

Performance analysis and operating potential of a hybrid-electric regional aircraft with box-wing lifting architecture Abstract: The payload-range diagram of a regional hybrid-electric box-wing aircraft is discussed in this paper. The operational characteristics of a hybrid-electric aircraft differ from those of an aircraft with traditional thermal propulsion. The shape of the payload-range diagram of the hybrid-electric […]

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Ph.D. Thesis “Development of design tools and methods for box-wing airplanes and application of the PrandtlPlane concept to a short-medium range aircraft” by Dr. Karim Abu Salem is now available on ETD portal.

This dissertation focuses on the study of the innovative PrandtlPlane aircraft. The PrandtlPlane is the application in aeronautical engineering of an unconventional aerodynamic concept based on the Best Wing System theory, postulated by Prandtl one century ago; the lifting system of this configuration is a box-wing properly designed to minimise the induced drag. The study […]

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A new paper published in Aerospace (MDPI): “A Physics-Based Multidisciplinary Approach for the Preliminary Design and Performance Analysis of a Medium Range Aircraft with Box-Wing Architecture” (Open Access)

  The introduction of disruptive innovations in the transport aviation sector is becoming increasingly necessary. This is because there are many very demanding challenges that the transport aviation system will have to face in the years ahead. In particular, the reduction in pollutant emissions from air transport, and its impact on climate change, clearly must […]

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A new paper published in Aerotecnica Missili & Spazio (Springer): “Preliminary Take-Off Analysis and Simulation of PrandtlPlane Commercial Aircraft” (Open Access)

The present paper deals with the take-off performance analysis of PrandtlPlane aircraft. The PrandtlPlane is a Box-Wing configuration based on Prandtl’s “Best Wing System” concept, which minimizes the induced drag once wingspan and lift are given. The take-off dynamics is simulated implementing the non-linear equations of motion in a numerical tool, which adopts a Vortex […]

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