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Static Analysis Settings No. 1 - Large deformations | Newton-Raphson | 500 | 1 Infinity Norm 9.00e+09 -- Stiffness matrix determinant 2.17e+6899 -- 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 11 Calculation statistic Maximum rotation about Z-axis 0.0 mrad Maximum rotation about Y-axis 16.0 mrad Member No. 1, x: 18.330000 ft Maximum rotation about X-axis 10.9 mrad Member No. 1, x: 18.330000 ft Maximum vectorial displacement 63.540 in FE node No. 210: (8.004936, 13.323567, 15.000000 ft) Maximum displacement in Z-direction -63.523 in FE node No. 210: (8.004936, 13.323567, 15.000000 ft) Maximum displacement in Y-direction -38.158 in Member No. 6, x: 16.695105 ft Maximum displacement in X-direction 33.919 in Member No. 5, x: 12.591175 ft Maximum deformations Resultant of reactions about Z -0.40 kipft At center of gravity of model Resultant of reactions about Y -5.19 kipft At center of gravity of model Resultant of reactions about X -3.04 kipft At center of gravity of model (8.256732, 12.812667, 7.990012 ft) Resultant of reactions Sum of support forces in Z -7.632 kip Deviation: 0.00 % Sum of loads in Z -7.632 kip Sum of support forces in Y 0.017 kip Deviation: 0.00 % Sum of loads in Y 0.017 kip Sum of support forces in X -0.613 kip Deviation: 0.00 % Sum of loads in X -0.613 kip Sum of loads and sum of support forces 3 CO10 - 1.20D + 0.50W4 + 1.60Lr 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 8.89e+09 -- Stiffness matrix determinant 3.03e+6734 -- 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 8 Calculation statistic Maximum rotation about Z-axis 0.0 mrad Maximum rotation about Y-axis -7.5 mrad Member No. 2, x: 18.330000 ft Maximum rotation about X-axis 5.1 mrad Member No. 1, x: 18.330000 ft Maximum vectorial displacement 44.466 in FE node No. 210: (8.004936, 13.323567, 15.000000 ft) Maximum displacement in Z-direction -44.419 in FE node No. 210: (8.004936, 13.323567, 15.000000 ft) Maximum displacement in Y-direction -37.011 in Member No. 6, x: 16.695105 ft Maximum displacement in X-direction 32.726 in Member No. 5, x: 12.591175 ft Maximum deformations Resultant of reactions about Z 0.00 kipft At center of gravity of model Resultant of reactions about Y 0.08 kipft At center of gravity of model Resultant of reactions about X 0.36 kipft At center of gravity of model (8.256732, 12.812667, 7.990012 ft) Resultant of reactions Sum of support forces in Z -4.880 kip Deviation: 0.00 % Sum of loads in Z -4.880 kip Description Value Unit Notes