A number of numerical solution technologies were developed for advanced analysis capabilities involving the finite element method in advanced constitutive modeling and structural analysis for improved and rational designs of aerospace propulsive systems. These technologies were incorporated into several advanced viscoplastic models and were applied to a wide spectrum of structural engineering problems involving extremes of thermal/mechanical loading. Results of the research performed under the grant were presented at a number of scientific meetings and conferences and have resulted in numerous publications
A viscoplastic theory is developed that reduces analytically to creep theory under steady-state cond...
Several explicit integration algorithms with self-adative time integration strategies are developed ...
Nonlinear structural analysis techniques for engine structures and components are addressed. The fin...
The viability of advanced viscoplastic models for nonlinear finite element analyses of structural co...
The results are presented of a viscoplastic stress-strain analysis of a cylindrical thrust chamber u...
The time-dependent thermo-viscoplastic response of aerospace structures subjected to intense aerothe...
A brief description of the implementation in MARK, the general purpose finite element structural ana...
The objective of this research project was to develop robust and efficient computational tools for d...
A description of the finite element implementation of Robinson's unified viscoplastic model into the...
Typical High Temperature Applications High Temperature Applications Demand High Performance Material...
A thermoviscoplastic computational method for hypersonic structures is presented. The method employs...
The prediction of inelastic behavior of metallic materials at elevated temperatures has increased in...
Due to the stringent design requirement for aerospace or nuclear structural components, considerable...
Technique computes stresses resulting from axisymmetric transient thermal loading in circular solid-...
This document describes a recently developed analysis tool that enhances the resident capabilities o...
A viscoplastic theory is developed that reduces analytically to creep theory under steady-state cond...
Several explicit integration algorithms with self-adative time integration strategies are developed ...
Nonlinear structural analysis techniques for engine structures and components are addressed. The fin...
The viability of advanced viscoplastic models for nonlinear finite element analyses of structural co...
The results are presented of a viscoplastic stress-strain analysis of a cylindrical thrust chamber u...
The time-dependent thermo-viscoplastic response of aerospace structures subjected to intense aerothe...
A brief description of the implementation in MARK, the general purpose finite element structural ana...
The objective of this research project was to develop robust and efficient computational tools for d...
A description of the finite element implementation of Robinson's unified viscoplastic model into the...
Typical High Temperature Applications High Temperature Applications Demand High Performance Material...
A thermoviscoplastic computational method for hypersonic structures is presented. The method employs...
The prediction of inelastic behavior of metallic materials at elevated temperatures has increased in...
Due to the stringent design requirement for aerospace or nuclear structural components, considerable...
Technique computes stresses resulting from axisymmetric transient thermal loading in circular solid-...
This document describes a recently developed analysis tool that enhances the resident capabilities o...
A viscoplastic theory is developed that reduces analytically to creep theory under steady-state cond...
Several explicit integration algorithms with self-adative time integration strategies are developed ...
Nonlinear structural analysis techniques for engine structures and components are addressed. The fin...