A SIMPLE NONLINEAR-ANALYSIS OF MULTILAYERED RECTANGULAR-PLATES

[21] LEVY S, 1969, P S APPL MATH AMS, V1, P197

[22] MAU ST, 1972, NASA CR1936

[23] BASIS FOR DERIVATION OF MATRICES FOR THE DIRECT STIFFNESS METHOD [J]. AIAA JOURNAL, 1963, 1 (07) : 1631 - 1637

[24] BENDING OF THIN LAMINATED PLATES [J]. COMPUTERS & STRUCTURES, 1987, 25 (02) : 271 - 280

[25] MOTTRAM JT, 1984, THESIS DURHAM U

[26] HYBRID ANALYTICAL TECHNIQUE FOR NONLINEAR-ANALYSIS OF STRUCTURES [J]. AIAA JOURNAL, 1985, 23 (06) : 938 - 946

[27] NOOR AK, 1977, DEV COMPOSITE MATERI, P55

[28] NOOR AK, 1974, COMPUTING METHODS NO, P1

[29] COMPOSITES IN THE CONSTRUCTION OF THE LEAR FAN-2100 AIRCRAFT [J]. COMPOSITES, 1983, 14 (02): : 129 - 139

[30] ODEN JT, 1967, P AM SOC CIVIL ENG, V93, P235

[21] LEVY S, 1969, P S APPL MATH AMS, V1, P197

[22] MAU ST, 1972, NASA CR1936

[23] BASIS FOR DERIVATION OF MATRICES FOR THE DIRECT STIFFNESS METHOD [J]. AIAA JOURNAL, 1963, 1 (07) : 1631 - 1637

[24] BENDING OF THIN LAMINATED PLATES [J]. COMPUTERS & STRUCTURES, 1987, 25 (02) : 271 - 280

[25] MOTTRAM JT, 1984, THESIS DURHAM U

[26] HYBRID ANALYTICAL TECHNIQUE FOR NONLINEAR-ANALYSIS OF STRUCTURES [J]. AIAA JOURNAL, 1985, 23 (06) : 938 - 946

[27] NOOR AK, 1977, DEV COMPOSITE MATERI, P55

[28] NOOR AK, 1974, COMPUTING METHODS NO, P1

[29] COMPOSITES IN THE CONSTRUCTION OF THE LEAR FAN-2100 AIRCRAFT [J]. COMPOSITES, 1983, 14 (02): : 129 - 139

[30] ODEN JT, 1967, P AM SOC CIVIL ENG, V93, P235