The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 April 1961
Abstract
The general theory of the cut‐out and modification analysis is reviewed and extended for a structure involving primary, secondary and tertiary redundancies. Some important points of practical application are illustrated on simple examples and the influence of the form chosen for the unassembled flexibility matrix is discussed. The question of the selection and number of actual cuts which will simulate a given major cut‐out is treated in general and illustrated on a simple type of structure.
Citation
Argyris, J.H. and Kelsey, S. (1961), "The Analysis of Fuselages of Arbitrary Cross‐section and Taper: A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer", Aircraft Engineering and Aerospace Technology, Vol. 33 No. 4, pp. 103-113. https://doi.org/10.1108/eb033398
Publisher
:MCB UP Ltd
Copyright © 1961, MCB UP Limited