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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 1.27e+14 -- Stiffness matrix determinant 3.25e+13632 -- Minimum value of element of stiffness matrix on diagonal 100.00 -- Maximum value of element of stiffness matrix on diagonal 5.71e+13 -- Number of iterations 10 Calculation statistic Maximum rotation about Z-axis -0.1 mrad Member No. 4, x: 19.313500 ft Maximum rotation about Y-axis 7.5 mrad Member No. 5, x: 13.330000 ft Maximum rotation about X-axis -9.2 mrad Member No. 2, x: 19.330000 ft Maximum vectorial displacement 52.346 in Member No. 11, x: 21.496112 ft Maximum displacement in Z-direction -32.912 in FE node No. 163: (-14.226229, -12.006595, 15.920396 ft) Maximum displacement in Y-direction 50.679 in Member No. 11, x: 21.496112 ft Maximum displacement in X-direction -49.318 in Member No. 13, x: 20.689090 ft Maximum deformations Resultant of reactions about Z -4.97 kipft At center of gravity of model Resultant of reactions about Y -29.10 kipft At center of gravity of model Resultant of reactions about X -14.52 kipft At center of gravity of model (5.206824, -11.262029, 8.906877 ft) Resultant of reactions Sum of support forces in Z -5.231 kip Deviation: 0.00 % Sum of loads in Z -5.231 kip Sum of support forces in Y 0.249 kip Deviation: 0.00 % Sum of loads in Y 0.249 kip Sum of support forces in X 1.756 kip Deviation: 0.00 % Sum of loads in X 1.756 kip Sum of loads and sum of support forces 5 CO37 - D + 0.60W1 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 1.27e+14 -- Stiffness matrix determinant 2.42e+13917 -- Minimum value of element of stiffness matrix on diagonal 100.00 -- Maximum value of element of stiffness matrix on diagonal 5.71e+13 -- Number of iterations 11 Calculation statistic Maximum rotation about Z-axis 0.0 mrad Member No. 1, x: 0.000000 ft Maximum rotation about Y-axis 8.7 mrad FE node No. 5: (-7.162202, -33.018136, 19.000000 ft) Maximum rotation about X-axis -11.3 mrad Member No. 2, x: 19.330000 ft Maximum vectorial displacement 64.264 in FE node No. 620: (14.075309, -15.826300, 15.240000 ft) Description Value Unit Notes