Automated Method for the Large Deflection and Instability Analysis of Three-dimensional Truss and Frame Assemblies
R. H. Mallett · L. Berke
Jan 1966 · Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force
Ebook
64
Pages
About this ebook
The computer program presented in this report was developed to predict large deflection behavior of three-dimensional truss and frame assemblies. The solutions are obtained by the direct minimization of the total potential energy with respect to the displacement variables rather than by solving nonlinear matrix equations. Sample problems are presented to demonstrate the analysis capability developed. Instructions for the preparation of the input data and the Fortran IV source program listing are included.
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