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- W2074000930 abstract "The basic problem of a flapped NACA-16 foil is its poor pressure distribution around the flapped region. With the flap deflected, the velocity distribution becomes a very unfavorable shape in terms of cavitationinception and boundary-layer separation. This type of flow field results in low flap effectiveness. Based on the present profile design and boundary-layer calculation methods, improved hydrofoil wings with flaps have been developed. The approaches to construct the desired velocity distributions to delay cavitation and boundary-layer separation are discussed. Examples are given for the case that the flap deflection has to compensate the vertical component of the surface wave motion in a seaway." @default.
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- W2074000930 date "1979-04-01" @default.
- W2074000930 modified "2023-09-25" @default.
- W2074000930 title "Section Design for Hydrofoil Wings with Flaps" @default.
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- W2074000930 doi "https://doi.org/10.2514/3.63152" @default.
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