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The Estimation of Aerofoil Lifting Characteristics: The Derivation and Application of Methods Developed in the R.A.E.

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 September 1947

Abstract

THE lift coefficient of an aerofoil fitted with a hinged control flap and a tab can be expressed in the form:

Citation

Bisgood, F.P.L. (1947), "The Estimation of Aerofoil Lifting Characteristics: The Derivation and Application of Methods Developed in the R.A.E.", Aircraft Engineering and Aerospace Technology, Vol. 19 No. 9, pp. 278-286. https://doi.org/10.1108/eb031546

Publisher

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MCB UP Ltd

Copyright © 1947, MCB UP Limited