The objective of this research is to develop an analytical tool capable of economically evaluating the cyclic time dependent plasticity which occurs in hot section engine components in areas of strain concentration resulting from the combination of both mechanical and thermal stresses. The techniques developed must be capable of accommodating large excursions in temperatures with the associated variations in material properties including plasticity and creep. The overall objective of this proposed program is to develop advanced 3-D inelastic structural/stress analysis methods and solution strategies for more accurate and yet more cost effective analysis of combustors, turbine blades, and vanes. The approach will be to develop four different...
The structural analysis technologies and activities of the NASA Lewis Research Center's gas turbine ...
Simplified inelastic analysis procedures were developed at NASA Lewis and Pratt & Whitney Aircraft f...
The advantages of a newly developed code are demonstrated by comparisons of the analysis with existi...
Advanced 3-D inelastic structural/stress analysis methods and solution strategies for more accurate ...
The objective is to develop analytical tools capable of economically evaluating the cyclic time depe...
Advanced 3-D inelastic structural/stress analysis methods and solution strategies for more accurate ...
Three-dimensional Inelastic Analysis Methods are described. These methods were incorporated into a s...
Accomplishments are described for the 2-year program, to develop advanced 3-D inelastic structural s...
The objective of this program is to produce a series of new computer codes that permit more accurate...
The objective of this program is to produce a series of new computer codes that permit more accurate...
A 3-D inelastic analysis methods program consists of a series of computer codes embodying a progress...
A 3-D Inelastic Analysis Method program is described. This program consists of a series of new compu...
This annual status report presents the results of work performed during the fourth year of the 3-D I...
The goal is the development of an alternative stress analysis tool, distinct from the finite element...
This Annual Status Report presents the results of work performed during the third year of the 3-D In...
The structural analysis technologies and activities of the NASA Lewis Research Center's gas turbine ...
Simplified inelastic analysis procedures were developed at NASA Lewis and Pratt & Whitney Aircraft f...
The advantages of a newly developed code are demonstrated by comparisons of the analysis with existi...
Advanced 3-D inelastic structural/stress analysis methods and solution strategies for more accurate ...
The objective is to develop analytical tools capable of economically evaluating the cyclic time depe...
Advanced 3-D inelastic structural/stress analysis methods and solution strategies for more accurate ...
Three-dimensional Inelastic Analysis Methods are described. These methods were incorporated into a s...
Accomplishments are described for the 2-year program, to develop advanced 3-D inelastic structural s...
The objective of this program is to produce a series of new computer codes that permit more accurate...
The objective of this program is to produce a series of new computer codes that permit more accurate...
A 3-D inelastic analysis methods program consists of a series of computer codes embodying a progress...
A 3-D Inelastic Analysis Method program is described. This program consists of a series of new compu...
This annual status report presents the results of work performed during the fourth year of the 3-D I...
The goal is the development of an alternative stress analysis tool, distinct from the finite element...
This Annual Status Report presents the results of work performed during the third year of the 3-D In...
The structural analysis technologies and activities of the NASA Lewis Research Center's gas turbine ...
Simplified inelastic analysis procedures were developed at NASA Lewis and Pratt & Whitney Aircraft f...
The advantages of a newly developed code are demonstrated by comparisons of the analysis with existi...