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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

30

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

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MCB UP Ltd

Copyright © 1957, MCB UP Limited

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