Fuselage Interference Effect: The Available Data points to Conclusions Favourable to the High Wing in Monoplanes
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 August 1931
Abstract
IT has been found by model tests that the lift of a combination of an aeroplane body and a wing is not in general equal to the sum of the lifts of the two components when tested separately. This difference is broadly referred to as an interference effect. It is dependent on a number of factors which can be generalised into three groups:—
Citation
Hartshorn, A.S. (1931), "Fuselage Interference Effect: The Available Data points to Conclusions Favourable to the High Wing in Monoplanes", Aircraft Engineering and Aerospace Technology, Vol. 3 No. 8, pp. 201-203. https://doi.org/10.1108/eb037653
Publisher
:MCB UP Ltd
Copyright © 1931, MCB UP Limited