Recommendations for numerical solution of reinforced-panel and fuselage-ring problems
Description:
Report presenting procedures for solving the equations of equilibrium of reinforced panels and isolated fuselage rings as represented by the external loads and operations table established according to Southwell's method. By using these equations, the stress distribution can be easily determined.
Date:
December 1948
Creator:
Hoff, N. J. & Libby, Paul A.
Partner:
UNT Libraries Government Documents Department