Stresses in reinforcing rings due to axial forces in cylindrical and conical stressed skins
This is a 1938 NACA Technical Memorandum from the NASA Technical Reports Server, a government engineering report on stresses in reinforcing rings on cylindrical and conical aircraft skins, written for aeronautical engineers and researchers. Its pictures are plain black-and-white graphs of moment coefficients plotted as curve families across angles, alongside a few line diagrams of ring-reinforced tubes under axial load, offering a designer little beyond their dense technical charting style and the clean diagrammatic linework of stressed skin structures.
