Matrix Analysis of the Circular Conical Fuselage: A Development and Revision of an Earlier Paper to Include the case of Cut‐outs
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 February 1957
32
Abstract
THE strain energy (UF) in a frame is expressed by the equation
Citation
Goodey, W.J. (1957), "Matrix Analysis of the Circular Conical Fuselage: A Development and Revision of an Earlier Paper to Include the case of Cut‐outs", Aircraft Engineering and Aerospace Technology, Vol. 29 No. 2, pp. 47-55. https://doi.org/10.1108/eb032795
Publisher
:MCB UP Ltd
Copyright © 1957, MCB UP Limited