A CYLINDRICAL SHELL DISCRETE ELEMENT

[1] BEITCH L, 1966, 7TH P AIAA ASME STRU, P35

[2] BOGNER FK, 1966, TR6680 WRIGHT PATT A

[3] FULTON RE, 1966, 5TH P US C APPL MECH, P272

[4] ANALYSIS OF AXISYMMETRICAL SHELLS BY THE DIRECT STIFFNESS METHOD [J]. AIAA JOURNAL, 1963, 1 (10) : 2342 - 2347

[5] JONES RE, 1966, TR6680 WRIGHT PATT A

[6] STRUCTURAL ANALYSIS AND INFLUENCE COEFFICIENTS FOR DELTA-WINGS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (07): : 449 - 454

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

[8] A STIFFNESS MATRIX FOR THE ANALYSIS OF THIN PLATES IN BENDING [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (01): : 34 - 42

[9] PAPPENFUSS BW, 1959, THESIS U WASHINGTON

[10] DERIVATION OF ELEMENT STIFFNESS MATRICES BY ASSUMED STRESS DISTRIBUTIONS [J]. AIAA JOURNAL, 1964, 2 (07) : 1333 - 1336

[1] BEITCH L, 1966, 7TH P AIAA ASME STRU, P35

[2] BOGNER FK, 1966, TR6680 WRIGHT PATT A

[3] FULTON RE, 1966, 5TH P US C APPL MECH, P272

[4] ANALYSIS OF AXISYMMETRICAL SHELLS BY THE DIRECT STIFFNESS METHOD [J]. AIAA JOURNAL, 1963, 1 (10) : 2342 - 2347

[5] JONES RE, 1966, TR6680 WRIGHT PATT A

[6] STRUCTURAL ANALYSIS AND INFLUENCE COEFFICIENTS FOR DELTA-WINGS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (07): : 449 - 454

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

[8] A STIFFNESS MATRIX FOR THE ANALYSIS OF THIN PLATES IN BENDING [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (01): : 34 - 42

[9] PAPPENFUSS BW, 1959, THESIS U WASHINGTON

[10] DERIVATION OF ELEMENT STIFFNESS MATRICES BY ASSUMED STRESS DISTRIBUTIONS [J]. AIAA JOURNAL, 1964, 2 (07) : 1333 - 1336