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An Investigation of Hydrofoils in the NACA Tank I : Effect of Dihedral and Depth of SubmersionTests were conducted on hydrofoil assemblies approximating an arrangement for use under seaplanes or surface boats. A series of hydrofoils, each supported by two struts, was towed at various depths ranging from partial submersions to a depth of 5-chord lengths. At depths greater than 4 or 5 chords, the influence of the surface of the water is small; hydrofoils operating at low speed will have characteristics similar to those of airfoils of the same section.
Document ID
19930092993
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Wartime Report
External Source(s)
Authors
Land, Norman S.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Benson, James M.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1942
Subject Category
Aerodynamics
Report/Patent Number
NACA-WR-L-758
Accession Number
93R22283
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYDROFOILS - NACA - CHARACTERISTICS TANK TESTS (NACA) & WIND-TUNNEL TESTS (NACA)
WIND TUNNEL TESTS - NACA-HIGH-SPEED (2') LMAL
HYDROFOILS - CHARACTERISTICS EFFECT OF LEADING EDGE SHAPE
CAVITATIONS - WATER
HYDROFOILS - NACA 16-509 - CHAR
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