The invention relates to wing-in-ground-effect vehicles having an aerodynamic "composite wing" configuration. The technical result is an increase in safety by providing for the static, non-oscillatory and oscillatory stability of a wing-in-ground-effect vehicle, and a reduction in induced drag by delaying stalling on the panels of a composite wing in the region where said panels abut a centre section. The present wing-in-ground-effect vehicle has a composite wing having a centre section (1) and panels (2), end-plates (3) in the end sections of the centre section (1), a propulsion unit, a vertical stabilizer (4), and a horizontal stabilizer (5). The aspect ratio of the composite wing is λ=l
Wing-in-ground-effect vehicle
24.03.2022
Patent
Elektronische Ressource
Englisch
NTIS | 1977
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