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Investigation at Low Speeds of Deflectors and Spoilers as Gust Alleviators on a Model of the Bell X-5 Airplane with 35 Degree Swept Wings and on a High-aspect-ratio 35 Degree Swept-wing-fuselage ModelResults of an investigation at low speeds to determine the gust-alleviation capabilities (reduction in lift-curve slope) of spoilers and deflectors on a 35 degree swept-wing model of high aspect ratio and on a 1/4-scale model of the X-5 airplane with 35 degree swept wings indicate that deflector and spoiler-deflector types of controls can be designed to provide considerable gust alleviation for a swept-wing airplane while still maintaining stability and control.
Document ID
19930084891
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Croom, Delwin R
Huffman, Jarrett K
Date Acquired
August 16, 2013
Publication Date
June 1, 1957
Report/Patent Number
NACA-TN-4057
Report Number: NACA-TN-4057
Accession Number
93R14181
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CONTROLS, SPOILER - COMPLETE WINGS
STABILITY, LATERAL - STATIC
STABILITY, LONGITUDINAL - STATIC
LOADS, GUST - WINGS
GUSTS, ALLEVIATION
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