Transfer of End Load in Stringers: The Stress Distribution Problem of the Bending of a Fuselage with a Symmetrical Opening

Abstract

A GENERAL solution is obtained for the diffusion of stress in n equal and equally spaced stringers in a stiffened panel subject to any boundary conditions at the ends of the stringers.

Citation

Richards, E.J. (1939), "Transfer of End Load in Stringers: The Stress Distribution Problem of the Bending of a Fuselage with a Symmetrical Opening", Aircraft Engineering and Aerospace Technology, Vol. 11 No. 8, pp. 301-305. https://doi.org/10.1108/eb030524