An algorithm developed and incorporated into BOPACE for improving the convergence and accuracy of the inelastic stress-strain calculations is discussed. The implementation of separation of strains in the residual-force iterative procedure is defined. The elastic-plastic quantities used in the strain-space algorithm are defined and compared with previous quantities
Theory is stated in terms of increments of displacement and stress, and of instantaneous or accumula...
The application of a structural computer program for analysis of a thrust chamber liner is discussed...
Incremental method for shakedown analysis of the elastic perfectly plastic structures is based on th...
The BOPACE program (Boeing plastic analysis capability for engines) was developed to meet the need f...
The current BOPACE program is described as a nonlinear stress analysis program, which is based on a ...
A computer program for use with a thermal-elastic-plastic-creep structural analyzer is presented. Th...
A simplified inelastic analysis computer program (ANSYPM) was developed for predicting the stress-st...
A simplified inelastic analysis computer program was developed for predicting the stress-strain hist...
Strain redistribution corrections were developed for a simplified inelastic analysis procedure to ec...
A user's guide to the processor MN is presented. The processor MN is used to analyze systems in whic...
Strain redistribution corrections were developed for a simplified inelastic analysis procedure to ec...
Simplified inelastic analysis procedures were developed at NASA Lewis and Pratt & Whitney Aircraft f...
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
AGGIE 1 is a computer program for predicting the linear and nonlinear, static and dynamic structural...
Theory is stated in terms of increments of displacement and stress, and of instantaneous or accumula...
The application of a structural computer program for analysis of a thrust chamber liner is discussed...
Incremental method for shakedown analysis of the elastic perfectly plastic structures is based on th...
The BOPACE program (Boeing plastic analysis capability for engines) was developed to meet the need f...
The current BOPACE program is described as a nonlinear stress analysis program, which is based on a ...
A computer program for use with a thermal-elastic-plastic-creep structural analyzer is presented. Th...
A simplified inelastic analysis computer program (ANSYPM) was developed for predicting the stress-st...
A simplified inelastic analysis computer program was developed for predicting the stress-strain hist...
Strain redistribution corrections were developed for a simplified inelastic analysis procedure to ec...
A user's guide to the processor MN is presented. The processor MN is used to analyze systems in whic...
Strain redistribution corrections were developed for a simplified inelastic analysis procedure to ec...
Simplified inelastic analysis procedures were developed at NASA Lewis and Pratt & Whitney Aircraft f...
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
AGGIE 1 is a computer program for predicting the linear and nonlinear, static and dynamic structural...
Theory is stated in terms of increments of displacement and stress, and of instantaneous or accumula...
The application of a structural computer program for analysis of a thrust chamber liner is discussed...
Incremental method for shakedown analysis of the elastic perfectly plastic structures is based on th...