Invention Grant
US08109473B2 Slotted high lift aerofoils 有权
开槽高升力机翼

Slotted high lift aerofoils
Abstract:
A slotted aerofoil configuration is provided in which the leading element thereof is contoured to provide mild stall characteristics. A wing based partially or fully on such an aerofoil, an air vehicle including such wings, and a method for designing an aerofoil are also disclosed.
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