Tapered Spar Frames: An Approximate Method for the Determination of the Stresses in, and Deflections of, a Fuselage

Abstract

THE methods and formula outlined below are applicable to any shape of fuselage, but an elliptical one is assumed to serve as an illustration.

Citation

Kittelsen, H.M.J. (1941), "Tapered Spar Frames: An Approximate Method for the Determination of the Stresses in, and Deflections of, a Fuselage", Aircraft Engineering and Aerospace Technology, Vol. 13 No. 4, pp. 90-94. https://doi.org/10.1108/eb030756