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Effect of Aspect Ratio on the Low-Speed Lateral Control Characteristics of Untapered Low-Aspect-Ratio Wings Equipped with Flap and with Retractable AileronsA low-speed wind-tunnel investigation was made to determine the lateral control characteristics of a series of untapered low-aspect-ratio wings. Sealed flap ailerons of various spans and spanwise locations were investigated on unswept wings of aspect ratios 1.13, 1.13, 4.13, and 6.13; and various projections of 0.60-semispan retractable ailerons were investigated on the unsweptback wings of aspect ratios 1.13, 2.13, and 4.13 and on a 45 degree sweptback wing. The retractable ailerons investigated on the unswept wings spanned the outboard stations of each wing; whereas the plain and stepped retractable ailerons investigated on the sweptback wing were located at various spanwise stations. Design charts based on experimental results are presented for estimating the flap aileron effectiveness for low-aspect-ratio, untapered, unswept.
Document ID
19930092133
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Fischel, Jack
Naeseth, Rodger L
Hagerman, John R
O'Hare, William M
Date Acquired
September 6, 2013
Publication Date
January 1, 1952
Report/Patent Number
NACA-TR-1091
Report Number: NACA-TR-1091
Accession Number
93R21423
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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