BASIS FOR DERIVATION OF MATRICES FOR THE DIRECT STIFFNESS METHOD

[1] BENTHEM JP, 1961, S578 NAT AER ASTR RE

[2] DILL EH, 1960, SARM13 BOEING CO

[3] GRAFTON PE, 1962, SARM36 BOEING CO

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

[5] LUNDER CA, 1961, THESIS U WASHINGTON

[6] Martin H. C., 1961, TREND ENG, V13, P5

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

[8] EVALUATION OF SPAR MATRICES FOR STIFFNESS ANALYSES [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1958, 25 (09): : 537 - 543

[9] ORTEGA MA, 1960, SARM15 BOEING CO

[10] ORTEGA MA, 1960, SARM14 BOEING CO

[1] BENTHEM JP, 1961, S578 NAT AER ASTR RE

[2] DILL EH, 1960, SARM13 BOEING CO

[3] GRAFTON PE, 1962, SARM36 BOEING CO

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

[5] LUNDER CA, 1961, THESIS U WASHINGTON

[6] Martin H. C., 1961, TREND ENG, V13, P5

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

[8] EVALUATION OF SPAR MATRICES FOR STIFFNESS ANALYSES [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1958, 25 (09): : 537 - 543

[9] ORTEGA MA, 1960, SARM15 BOEING CO

[10] ORTEGA MA, 1960, SARM14 BOEING CO