SEARCH · Search NASA
Results for “finite element method”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Finite-element methods for noncollinear magnetism and spin-orbit coupling in real-space pseudopotential density functional theory
Not Available
Predicting long-term stress relaxation on Alloy 709 using the crystal plasticity finite element method
This report summarizes the results of physics-based, crystal plasticity simulations for the long-term stress relaxation behavior of Alloy 709. The purpose of the study was to provide insight into five key questions related to long-term behavior in high temperatures materials which are difficult or impossible to answer experimentally: (1) is there a threshold stress for long-term relaxation? (2) is there strain threshold for relaxation damage, below which significant damage does not accumulate? (3) does damage continue to accumulate as the material relaxes or will damage accumulation plateau under some loading conditions? (4) does stress relaxation loading inevitably lead to failure? and (5) which, if any, engineering models for relaxation damage accumulation reasonably match the simulation results? The report summarizes the numerical simulations used to address these five questions and provides at least partial answers to each question.
Modified Immersed Finite Element Method (mIFEM) For Explicit Eulerian to Explicit Lagrangian Coupling
Explore the source record for details and available documents.
INTERFACE MECHANICS FOR EXPLICIT EULERIAN TO EXPLICIT LAGRANGIAN COUPLING USING THE MODIFIED IMMERSED FINITE ELEMENT METHOD
Explore the source record for details and available documents.
Modeling the Direct Ink Write process using a sharp interface finite-element method
Explore the source record for details and available documents.
Modeling Direct Ink Write of sinusoidal patterns using the conformal decomposition finite element method
Explore the source record for details and available documents.
Using the conformal decomposition finite element method to model the Direct Ink Write process for sinusoidal extrusion patterns
Explore the source record for details and available documents.
Impact Modeling with Explicit Eulerian to Explicit Lagrangian Coupling Using the Modified Immersed Finite Element Method
Explore the source record for details and available documents.
A GPU-Enabled Higher Order Mixed Finite Element Method for Pulsed Power ICF Target Design
Explore the source record for details and available documents.
Bridging mathematical rigor and data scalability: Data-driven finite element method
Explore the source record for details and available documents.
A finite element method for nonaxisymmetric vibrations of pressurized shells of revolution partially filled with liquid.
Explore the source record for details and available documents.
Water impact analysis of space shuttle solid rocket motor by the finite element method
Preliminary analysis showed that the doubly curved triangular shell elements were too stiff for these shell structures. The doubly curved quadrilateral shell elements were found to give much improved results. A total of six load cases were analyzed in this study. The load cases were either those resulting from a static test using reaction straps to simulate the drop conditions or under assumed hydrodynamic conditions resulting from a drop test. The latter hydrodynamic conditions were obtained through an emperical fit of available data. Results obtained from a linear analysis were found to be consistent with results obtained elsewhere with NASTRAN and BOSOR. The nonlinear analysis showed that the originally assumed loads would result in failure of the shell structures. The nonlinear analysis also showed that it was useful to apply internal pressure as a stabilizing influence on collapse. A final analysis with an updated estimate of load conditions resulted in linear behavior up to full load.
A finite element method for potential aerodynamics around complex configurations
A general formulation for steady and oscillatory, subsonic and supersonic, potential linearized aerodynamic flow around complex configurations is presented. A linear integral equation relating the unknown potential on the surface of the body to the known downwash is used. The formulation is applied to the analysis of the flow field around wings and wing-body combinations. The surface is divided into small quadrilateral elements which are approximated with a hyperboloidal surface. The potential is assumed to be constant within each element. This yields a set of linear algebraic equations. The coefficients are evaluated analytically. Numerical results for steady and oscillatory, subsonic and supersonic flows indicate that the method, intrinsically general and flexible, is also fast, accurate and in excellent agreement with existing results.
A finite-element method for lifting surfaces in steady incompressible subsonic flow
The problem of potential steady subsonic flow for lifting surfaces is considered. This problem requires the solution of an integral equation relating the value of the potential discontinuity on the lifting surface and its wake to the values of the normal derivative of the potential which are known from the boundary conditions. The lifting surface is divided into small (quadrilateral hyperboloidal) surface elements, which are described in terms of the Cartesian components of the four corner points. The values of the potential discontinuity and the normal derivative of the potential are assumed to be constant within each element and equal to their values at the centroids of the elements. This yields a set of linear algebraic equations. Numerical results are in good agreement with existing ones.
Some inconsistencies of the finite element method as applied to inelastic response
The inadequacy of a two noded beam-column element with a linear axial and a cubic transverse displacement field for inelastic analysis is demonstrated. For complete equilibrium satisfaction in the linear elastic range a three noded beam-column element is shown to be consistent. Next, the sensitivity of the inelastic response to numerical solutions of the inelastic response of a cantilever beam resulting from approximate integration of strain energy are brought out and finally, consequences of this on the nonlinear transient response of structures are considered.
N-person differential games. Part 1: Duality-finite element methods
The duality approach, which is motivated by computational needs and is done by introducing N + 1 Language multipliers is addressed. For N-person linear quadratic games, the primal min-max problem is shown to be equivalent to the dual min-max problem.
Fillet Weld Stress Using Finite Element Methods
Average elastic Von Mises equivalent stresses were calculated along the throat of a single lap fillet weld. The average elastic stresses were compared to initial yield and to plastic instability conditions to modify conventional design formulas is presented. The factor is a linear function of the thicknesses of the parent plates attached by the fillet weld.