The Analysis of Fuselages of Arbitrary Cross‐section and Taper
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 April 1959
Abstract
A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer. The present issue gives a summary of the basic theory of the matrix force method together with some necessary extensions for the fuselage problem. The equilibrium conditions for the idealized structure are then examined in detail and the relevant equations of equilibrium established in matrix form.
Citation
Argyris, J.H. and Kelsey, S. (1959), "The Analysis of Fuselages of Arbitrary Cross‐section and Taper", Aircraft Engineering and Aerospace Technology, Vol. 31 No. 4, pp. 101-112. https://doi.org/10.1108/eb033102
Publisher
:MCB UP Ltd
Copyright © 1959, MCB UP Limited