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Effects of a sweptback hydrofoil on the force and longitudinal stability characteristics of a typical high-speed airplaneAn investigation was conducted in the Langley 8-foot high-speed tunnel to determine the effects of a sweptback hydrofoil on the force and longitudinal stability characteristics of a typical high-speed airplane. The Mach number range for this investigation was from 0.60 to 0.95 and at M = 1.20. The effects of the hydrofoil on the lift, drag, and pitching-moment characteristics are presented.
Document ID
19930085476
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wood, Raymond B
Date Acquired
August 29, 2013
Publication Date
December 2, 1948
Report/Patent Number
NACA-RM-L8I30a
Report Number: NACA-RM-L8I30a
Accession Number
93R14766
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRPLANES - COMPONENTS IN COMBINATION
STABILITY, LONGITUDINAL - STATIC
AIRPLANES - SPECIFIC TYPES
HYDROFOILS

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