Nicholas John Hoff

A Survey of the Theories of Creep Buckling

Monocoque, Sandwich, and Composite Aerospace Structures

Stresses in a Space Curved Bar Reinforcing the Edge of a Cut-out in a Monocoque Fuselage

Paul A. Libby

Bertram Klein

Formulas for the calculation of influence coefficients of curved beams of constant radius of curvature are presented corresponding to displacements in the plane of curvature. Moreover, numerical values are given in tabular and graphicform for a limited number of values of the parameters involved.

Influence coefficients of curved bars for distortions in their own plane. IV

Numerical Procedures for the Calculation of Stresses in Monocoques

Harry Kase

Harold Liebowitz

The stresses in the two spars of a model of a wing having three rectangular cutouts were calculated by the PIBAL method, a modification of Southwell's method of systematic relaxations. The model was built and tested in the Polytechnic Institute of Brooklyn Aeronautical Laboratories and the deflections and strains measured were compared with calculated values. The agreement was found to be satisfactory.

Interaction Between the Spars of Semimonocoque Wings with Cutouts

Nicholas John Hoff

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