Study made in Langley tank to determine lift, drag, and pitching-moment characteristics of three hydrofoils, two triangular and one rectangular; triangular hydrofoil with leading-edge sweep had better overall lift drag ratios; maximum lift-drag ratio obtained was 5.0; pertinence to use of hydrofoil as landing gear for waterbased aircraft.
Force investigation of three surface-piercing supercavitating hydrofoils with 45° negative dihedral
NASA -- Tech Note
1960
44 pages
Report
English
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