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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 10.00e+6828 -- 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 -11.9 mrad Member No. 2, x: 18.330000 ft Maximum rotation about X-axis 7.5 mrad Member No. 1, x: 18.330000 ft Maximum vectorial displacement 55.710 in FE node No. 211: (8.643770, 11.991210, 15.000000 ft) Maximum displacement in Z-direction -55.693 in FE node No. 211: (8.643770, 11.991210, 15.000000 ft) Maximum displacement in Y-direction -38.033 in Member No. 6, x: 16.695105 ft Maximum displacement in X-direction 34.515 in Member No. 5, x: 12.591175 ft Maximum deformations Resultant of reactions about Z -1.11 kipft At center of gravity of model Resultant of reactions about Y 5.47 kipft At center of gravity of model Resultant of reactions about X 5.02 kipft At center of gravity of model (8.256732, 12.812667, 7.990012 ft) Resultant of reactions Sum of support forces in Z -6.001 kip Deviation: 0.00 % Sum of loads in Z -6.001 kip Sum of support forces in Y 0.000 kip Sum of loads in Y 0.000 kip Sum of support forces in X 0.611 kip Deviation: 0.00 % Sum of loads in X 0.611 kip Sum of loads and sum of support forces 3 CO2 - 1.20D + 0.50W1 + 1.60S 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 8.81e+09 -- Stiffness matrix determinant 7.81e+6393 -- 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 5 Calculation statistic Maximum rotation about Z-axis 0.0 mrad Maximum rotation about Y-axis -1.3 mrad Member No. 2, x: 18.330000 ft Maximum rotation about X-axis 0.9 mrad Member No. 1, x: 18.330000 ft Description Value Unit Notes