A new paper published in Aerotecnica Missili & Spazio (Springer): “Aerodynamic design of a light amphibious PrandtlPlane: wind tunnel tests and CFD validation”

As part of the activities carried out during the “IDINTOS” project, wind tunnel tests have been performed on a 1/4 scaled model of a two seats amphibious PrandtlPlane. The present paper deals with the CFD analyses performed after such experimental activities, with the main goal of solving lateral-directional stability problems observed during wind tunnel tests. […]

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