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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 8.15e+13879 -- 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 7.2 mrad Member No. 5, x: 13.330000 ft Maximum rotation about X-axis -10.7 mrad Member No. 2, x: 19.330000 ft Maximum vectorial displacement 59.009 in FE node No. 597: (17.139287, -14.119971, 15.243333 ft) Maximum displacement in Z-direction -58.811 in FE node No. 596: (15.682394, -14.256809, 15.251667 ft) Maximum displacement in Y-direction 50.777 in Member No. 11, x: 18.189018 ft Maximum displacement in X-direction -49.616 in Member No. 13, x: 22.280559 ft Maximum deformations Resultant of reactions about Z -0.98 kipft At center of gravity of model Resultant of reactions about Y 11.95 kipft At center of gravity of model Resultant of reactions about X 13.74 kipft At center of gravity of model (5.206824, -11.262029, 8.906877 ft) Resultant of reactions Sum of support forces in Z -10.228 kip Deviation: 0.00 % Sum of loads in Z -10.228 kip Sum of support forces in Y 1.051 kip Deviation: 0.00 % Sum of loads in Y 1.051 kip Sum of support forces in X 0.248 kip Deviation: 0.00 % Sum of loads in X 0.248 kip Sum of loads and sum of support forces 6 CO51 - D + 0.45W5 + 0.75Lr 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 4.88e+13767 -- 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 0.0 mrad Member No. 4, x: 19.313500 ft Maximum rotation about Y-axis 7.5 mrad Member No. 2, x: 19.330000 ft Maximum rotation about X-axis -8.2 mrad Member No. 2, x: 19.330000 ft Maximum vectorial displacement 57.284 in FE node No. 644: (12.443192, -17.374739, 15.278333 ft) Maximum displacement in Z-direction -57.071 in FE node No. 644: (12.443192, -17.374739, 15.278333 ft) Maximum displacement in Y-direction 49.694 in Member No. 11, x: 18.189018 ft Maximum displacement in X-direction -50.865 in Member No. 13, x: 22.280559 ft Maximum deformations Description Value Unit Notes