The current BOPACE program is described as a nonlinear stress analysis program, which is based on a family of isoparametric finite elements. The theoretical, user, programmer, preprocessing aspects are discussed, and example problems are included. New features in the current program version include substructuring, an out-of-core Gauss wavefront equation solver, multipoint constraints, combined material and geometric nonlinearities, automatic calculation of inertia effects, provision for distributed as well as concentrated mechanical loads, follower forces, singular crack-tip elements, the SAIL automatic generation capability, and expanded user control over input quantity definition, output selection, and program execution. BOPACE is written...
Simplified inelastic analysis procedures were developed at NASA Lewis and Pratt & Whitney Aircraft f...
A number of numerical solution technologies were developed for advanced analysis capabilities involv...
Nonlinear finite element analysis techniques are evaluated by applying them to a realistic aircraft ...
The BOPACE program (Boeing plastic analysis capability for engines) was developed to meet the need f...
A computer program for use with a thermal-elastic-plastic-creep structural analyzer is presented. Th...
An algorithm developed and incorporated into BOPACE for improving the convergence and accuracy of th...
Modifications and additions incorporated into the BOPACE 3-D program are described. Updates to the p...
AGGIE 1 is a computer program for predicting the linear and nonlinear, static and dynamic structural...
A simplified inelastic analysis computer program was developed for predicting the stress-strain hist...
Nonlinear structural analysis techniques for engine structures and components are addressed. The fin...
An evaluation of the ACTION computer code on an aircraft like structure is presented. This computer ...
Finite element method computer program for solution of stress distribution in plane elastic continu
A simplified inelastic analysis computer program (ANSYPM) was developed for predicting the stress-st...
The APAS program a multistation structural synthesis procedure developed to evaluate material, geome...
The PLANS system, rather than being one comprehensive computer program, is a collection of finite el...
Simplified inelastic analysis procedures were developed at NASA Lewis and Pratt & Whitney Aircraft f...
A number of numerical solution technologies were developed for advanced analysis capabilities involv...
Nonlinear finite element analysis techniques are evaluated by applying them to a realistic aircraft ...
The BOPACE program (Boeing plastic analysis capability for engines) was developed to meet the need f...
A computer program for use with a thermal-elastic-plastic-creep structural analyzer is presented. Th...
An algorithm developed and incorporated into BOPACE for improving the convergence and accuracy of th...
Modifications and additions incorporated into the BOPACE 3-D program are described. Updates to the p...
AGGIE 1 is a computer program for predicting the linear and nonlinear, static and dynamic structural...
A simplified inelastic analysis computer program was developed for predicting the stress-strain hist...
Nonlinear structural analysis techniques for engine structures and components are addressed. The fin...
An evaluation of the ACTION computer code on an aircraft like structure is presented. This computer ...
Finite element method computer program for solution of stress distribution in plane elastic continu
A simplified inelastic analysis computer program (ANSYPM) was developed for predicting the stress-st...
The APAS program a multistation structural synthesis procedure developed to evaluate material, geome...
The PLANS system, rather than being one comprehensive computer program, is a collection of finite el...
Simplified inelastic analysis procedures were developed at NASA Lewis and Pratt & Whitney Aircraft f...
A number of numerical solution technologies were developed for advanced analysis capabilities involv...
Nonlinear finite element analysis techniques are evaluated by applying them to a realistic aircraft ...