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Finite element method analysis of axisymmetrically loaded thin shells of revolution, considering nonlinearity due to material properties and shell geometry changes
Natural vibration frequencies and mode shapes for laminated orthotropic shells of revolution using finite element method
Discrete models for boundary value problems analysis in first strain-gradient elasticity theory, using extended finite element method
Plates elastic-plastic behavior under combined stretching and bending by finite element method
Two dimensional structures large strain elastoplastic analysis by finite element method, using variational principles to derive equilibrium equations
Axisymmetric postyielded tongue and groove cylindrical joint stress analysis using finite element method
Stress and vibration analysis of rocket engine turboprop inducer blades, using finite element method
Structure of flexural members, analyzing torsional and lateral stability by finite element method and matrix formulation
Computer program, CRAB, uses finite-element method to calculate creep behavior and predict steady-state stresses in an arbitrary body of revolution subjected to a time-dependent axisymmetric load. Creep strains follow a time hardening law and a Prandtl-Reuss stress-strain relationship.
Description of general purpose digital computer program /NASTRAN/ for analysis of elastic structures under various loading conditions using finite element method approach
Manipulation errors in computer solution of critical size structural equations using finite element method
Reduction of proliferation and maintainability of finite element method computer programs
Edge cracked metal sheet elastoplastic strain distribution determination, using optical interference, moire technique and plane stress model finite element method
Kernel function for nonplanar oscillating surfaces in supersonic flow, using finite element method for interfering configurations
Elastic shells of revolution displacement analysis, using incremental variational theory with finite element method
A procedure cast in a form appropriate to the finite element method is presented for geometrically nonlinear prebuckling and postbuckling structural analysis, including the identification of snap-through type of buckling. The principal features of this procedure are the use of direct iteration for solution of the nonlinear algebraic equations in the prebuckling range, an interpolation scheme for determination of the initial bifurcation point, a perturbation method in definition of the load-displacement behavior through the postbuckling regime, and extrapolation in determination of the limit point for snap-through buckling. Three numerical examples are presented in illustration of the procedure and in comparison with alternative approaches.
A large deflection elastic-plastic analysis is presented, applicable to orthotropic axisymmetric plates and shells of revolution subjected to monotonic and cyclic loading conditions. The analysis is based on the finite-element method. It employs a new higher order, fully compatible, doubly curved orthotropic shell-of-revolution element using cubic Hermitian expansions for both meridional and normal displacements. Both perfectly plastic and strain hardening behavior are considered. Strain hardening is incorporated through use of the Prager-Ziegler kinematic hardening theory, which predicts an ideal Bauschinger effect. Numerous sample problems involving monotonic and cyclic loading conditions are analyzed. The monotonic results are compared with other theoretical solutions.
A general analysis of dynamic systems consisting of connected rigid bodies is presented. The number of bodies and their manner of connection is arbitrary so long as no closed loops are formed. The analysis represents a dynamic finite element method, which is computer-oriented and designed so that nonworking, interval constraint forces are automatically eliminated. The method is based upon Lagrange's form of d'Alembert's principle. Shifter matrix transformations are used with the geometrical aspects of the analysis. The method is illustrated with a space manipulator.