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A Physics-Based Multidisciplinary Approach for the Preliminary Design and Performance Analysis of a Medium Range Aircraft with Box-Wing Architecture

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Aircraft Hybrid-Electric Propulsion: Development Trends, Challenges and Opportunities

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A Conceptual Design Methodology for e-VTOL Aircraft for Urban Air Mobility

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Prediction of Maximum Lift Coefficient of Box-Wing Aircraft through the Combination of an Analytical Adaptation of the DATCOM Method and Vortex-Lattice Simulations

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Journal of Aerospace Engineering 35 (3) (2022)
DOI: 10.1061/(ASCE)AS.1943-5525.0001409
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Tools and methodologies for box-wing aircraft conceptual aerodynamic design and aeromechanic analysis

Karim Abu Salem, Palaia Giuseppe, Cipolla Vittorio, Binante Vincenzo, Zanetti Davide, Chiarelli Mario, Joseph Morlier and Michael Kokkolaras
Mechanics & Industry 22 39 (2021)
DOI: 10.1051/meca/2021037
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