Matrix Analysis of the Circular Conical Fuselage: A Development and Revision of an Earlier Paper to Include the case of Cut‐outs

Abstract

IN this part we shall consider the effect of non‐uniformity (with respect to k) in the longitudinal members, with particular reference to the case of four longerons, and we shall then go on to discuss the treatment of cut‐outs.

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. 3, pp. 77-88. https://doi.org/10.1108/eb032806