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Static Analysis Settings No. 1 - Large deformations | Newton-Raphson | 500 | 1 Infinity Norm 8.93e+09 -- Stiffness matrix determinant 2.98e+6799 -- Minimum value of element of stiffness matrix on diagonal 100.00 -- Maximum value of element of stiffness matrix on diagonal 4.40e+09 -- Number of iterations 10 Calculation statistic Maximum rotation about Z-axis 0.0 mrad Maximum rotation about Y-axis 10.3 mrad Member No. 1, x: 18.330000 ft Maximum rotation about X-axis 7.1 mrad Member No. 1, x: 18.330000 ft Maximum vectorial displacement 52.791 in FE node No. 229: (5.901263, 14.722119, 15.047368 ft) Maximum displacement in Z-direction -52.678 in FE node No. 230: (6.542417, 13.383744, 15.015789 ft) Maximum displacement in Y-direction 37.485 in Member No. 8, x: 16.172859 ft Maximum displacement in X-direction 33.099 in Member No. 5, x: 12.591175 ft Maximum deformations Resultant of reactions about Z -0.80 kipft At center of gravity of model Resultant of reactions about Y -10.72 kipft At center of gravity of model Resultant of reactions about X -7.84 kipft At center of gravity of model (8.256732, 12.812667, 7.990012 ft) Resultant of reactions Sum of support forces in Z -5.180 kip Deviation: 0.00 % Sum of loads in Z -5.180 kip Sum of support forces in Y 0.033 kip Deviation: 0.00 % Sum of loads in Y 0.033 kip Sum of support forces in X -1.225 kip Deviation: 0.00 % Sum of loads in X -1.225 kip Sum of loads and sum of support forces 4 CO27 - 1.20D + W4 + 0.50Lr Speed of convergence 1.00 -- Integrate preliminary form-finding Number of iterations for loading prestress 15 Plate bending theory Mindlin Method for Equation System Direct Try to calculate unstable structure Consider favorable effects due to tension forces of members Divide results by load factor Multiplier factor 1.00 -- Modify loading by multiplier factor Number of load increments 1 Maximum number of iterations 500 Iterative method Newton-Raphson Analysis type Large deformations Static Analysis Settings No. 1 - Large deformations | Newton-Raphson | 500 | 1 Infinity Norm 8.94e+09 -- Stiffness matrix determinant 3.86e+6843 -- Minimum value of element of stiffness matrix on diagonal 100.00 -- Maximum value of element of stiffness matrix on diagonal 4.40e+09 -- Number of iterations 10 Calculation statistic Maximum rotation about Z-axis 0.0 mrad Maximum rotation about Y-axis 11.5 mrad Member No. 1, x: 18.330000 ft Maximum rotation about X-axis -9.3 mrad Member No. 3, x: 12.330000 ft Maximum vectorial displacement 43.489 in Member No. 6, x: 16.695105 ft Maximum displacement in Z-direction 35.206 in FE node No. 231: (7.183570, 12.045370, 14.984211 ft) Maximum displacement in Y-direction -39.840 in Member No. 6, x: 15.177368 ft Maximum displacement in X-direction 37.567 in Member No. 5, x: 14.165072 ft Maximum deformations Resultant of reactions about Z 0.00 kipft At center of gravity of model Resultant of reactions about Y -0.18 kipft At center of gravity of model Resultant of reactions about X -1.02 kipft At center of gravity of model (8.256732, 12.812667, 7.990012 ft) Resultant of reactions Sum of support forces in Z 0.381 kip Deviation: 0.00 % Sum of loads in Z 0.381 kip Description Value Unit Notes