SENSITIVITY CALCULATIONS FOR ITERATIVELY SOLVED PROBLEMS

[1] DESIGN FOR TEMPERATURE AND THERMAL BUCKLING CONSTRAINTS EMPLOYING A NONEIGENVALUE FORMULATION [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1983, 20 (04) : 363 - 367

[2] TECHNIQUES FOR THERMAL SENSITIVITY ANALYSIS [J]. INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 1981, 17 (01) : 71 - 80

[3] CALCULATION OF SENSITIVITY DERIVATIVES IN THERMAL PROBLEMS BY FINITE-DIFFERENCES [J]. INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 1981, 17 (12) : 1811 - 1821

[4] HUGHES TJR, 1983, JUN ASME APPL MECH B

[5] MIURA H, 1979, NASA CR159070

[1] DESIGN FOR TEMPERATURE AND THERMAL BUCKLING CONSTRAINTS EMPLOYING A NONEIGENVALUE FORMULATION [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1983, 20 (04) : 363 - 367

[2] TECHNIQUES FOR THERMAL SENSITIVITY ANALYSIS [J]. INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 1981, 17 (01) : 71 - 80

[3] CALCULATION OF SENSITIVITY DERIVATIVES IN THERMAL PROBLEMS BY FINITE-DIFFERENCES [J]. INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 1981, 17 (12) : 1811 - 1821

[4] HUGHES TJR, 1983, JUN ASME APPL MECH B

[5] MIURA H, 1979, NASA CR159070