ANALYSIS OF AXISYMMETRICAL SHELLS BY THE DIRECT STIFFNESS METHOD

[1] GREENE BE, 1961, 61AV58 AM SOC MECH E

[2] CONICAL SEGMENT METHOD FOR ANALYZING OPEN CROWN SHELLS OF REVOLUTION FOR EDGE LOADING [J]. AIAA JOURNAL, 1963, 1 (04) : 886 - 891

[3] STIFFNESS AND DEFLECTION ANALYSIS OF COMPLEX STRUCTURES [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (09): : 805 - &

[4] LARGE DEFLECTIONS OF STRUCTURES SUBJECTED TO HEATING AND EXTERNAL LOADS [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (02): : 97 - &

[5] TURNER MJ, D222061 BOEING DOC

[6] TURNER MJ, 1962, JUL AGARD STRUCT MAT

[7] WEIKEL RC, 1962, ASDTDR62156 AER SYST

[1] GREENE BE, 1961, 61AV58 AM SOC MECH E

[2] CONICAL SEGMENT METHOD FOR ANALYZING OPEN CROWN SHELLS OF REVOLUTION FOR EDGE LOADING [J]. AIAA JOURNAL, 1963, 1 (04) : 886 - 891

[3] STIFFNESS AND DEFLECTION ANALYSIS OF COMPLEX STRUCTURES [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (09): : 805 - &

[4] LARGE DEFLECTIONS OF STRUCTURES SUBJECTED TO HEATING AND EXTERNAL LOADS [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (02): : 97 - &

[5] TURNER MJ, D222061 BOEING DOC

[6] TURNER MJ, 1962, JUL AGARD STRUCT MAT

[7] WEIKEL RC, 1962, ASDTDR62156 AER SYST