NONLINEAR VIBRATION OF SIMPLY SUPPORTED ANGLE PLY LAMINATED PLATES

[1] A MULTIPLE DEGREE-OF-FREEDOM APPROACH TO NONLINEAR BEAM VIBRATIONS [J]. AIAA JOURNAL, 1970, 8 (04) : 734 - &

[2] BERGER HM, 1965, J APPL MECH, V22, P465

[3] Chu H-N, 1956, J APPLIED MECHANICS, V23, P532

[4] HEARMON RF, 1961, INTRO APPL ANISOTROP, P12

[5] MAYBERRY BL, 1969, 39 SHOCK VIBR B 3, P277

[6] ON GENERAL THEORY OF HETEROGENEOUS AEOLOTROPIC PLATES [J]. AERONAUTICAL QUARTERLY, 1964, 15 (01): : 29 - &

[7] Stavsky Y, 1961, J ENG MECH, V87, P31

[8] STOKER JJ, 1950, NONLINEAR VIBRATIONS, pCH6

[9] TSAI SW, 1970, PRIVATE COMMUNICATIO

[10] Wah T., 1963, INT J MECH SCI, V5, P425, DOI DOI 10.1016/0020-7403(63)90026-2

[1] A MULTIPLE DEGREE-OF-FREEDOM APPROACH TO NONLINEAR BEAM VIBRATIONS [J]. AIAA JOURNAL, 1970, 8 (04) : 734 - &

[2] BERGER HM, 1965, J APPL MECH, V22, P465

[3] Chu H-N, 1956, J APPLIED MECHANICS, V23, P532

[4] HEARMON RF, 1961, INTRO APPL ANISOTROP, P12

[5] MAYBERRY BL, 1969, 39 SHOCK VIBR B 3, P277

[6] ON GENERAL THEORY OF HETEROGENEOUS AEOLOTROPIC PLATES [J]. AERONAUTICAL QUARTERLY, 1964, 15 (01): : 29 - &

[7] Stavsky Y, 1961, J ENG MECH, V87, P31

[8] STOKER JJ, 1950, NONLINEAR VIBRATIONS, pCH6

[9] TSAI SW, 1970, PRIVATE COMMUNICATIO

[10] Wah T., 1963, INT J MECH SCI, V5, P425, DOI DOI 10.1016/0020-7403(63)90026-2