Lift Correction for Finite Chord

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 June 1950

Abstract

IT has been noted by Falkner and others that the ordinary aspect‐ratio corrections based on lifting‐line theory are not as accurate as had always been assumed even for normal aspect ratios of the order of 6. Lifting‐surface theory involves heavy calculation, and the present work is intended to give at least an indication of the magnitude of the finite‐chord correction on a fairly simple basis.

Citation

Lockwood Taylor, J. (1950), "Lift Correction for Finite Chord", Aircraft Engineering and Aerospace Technology, Vol. 22 No. 6, pp. 174-174. https://doi.org/10.1108/eb031910

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Publisher

:

MCB UP Ltd

Copyright © 1950, MCB UP Limited

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