Investigation on rotating ailerons

Mozumdar, S and Patel, TS (1980) Investigation on rotating ailerons. Aeronautical Society of India, Journal, 32. pp. 1-5.

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Abstract

The effectiveness of rotating ailerons in a subsonic flow is theoretically studied to evaluate their capability in comparison to conventional ailerons. The analysis is based on the cortex lattice approach of Byelotserkovskii (1965) for different wing planforms of small and large aspect ratios. The rolling moment coefficient obtained with the rotating ailerons with a span equal to 22% of the wing span is higher than that for the conventional ailerons of almost double the span. The effectiveness of the rotating ailerons decreases with reduction in the wing aspect ratio, although it is possible to reduce the aileron size for required rolling capability

Item Type: Article
Uncontrolled Keywords: Control surfaces;Wings (aircraft);Rolling;Aspect ratio;Aeronautics;Coefficients;Lattices;Subsonic aircraft;Ailerons;Rotating bodies;Subsonic flow;Aerodynamic coefficients;Computational fluid dynamics;Lift;Rolling moments;Wing span
Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
AERONAUTICS > Aerodynamics
Depositing User: Users 11 not found.
Date Deposited: 01 Feb 2006
Last Modified: 24 May 2010 04:10
URI: http://nal-ir.nal.res.in/id/eprint/1052

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