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
:MCB UP Ltd
Copyright © 1947, MCB UP Limited