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Minimum value of element of stiffness matrix on diagonal 100.00 -- <br />Maximum value of element of stiffness matrix on diagonal 4.40e+09 -- <br />Number of iterations 9 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis -10.3 mrad Member No. 2, x: 18.330000 ft <br />Maximum rotation about X-axis 6.4 mrad Member No. 1, x: 18.330000 ft <br />Maximum vectorial displacement 52.422 in FE node No. 192: (10.740486, 10.610712, 15.047368 ft) <br />Maximum displacement in Z-direction -52.377 in FE node No. 192: (10.740486, 10.610712, 15.047368 ft) <br />Maximum displacement in Y-direction -38.443 in Member No. 6, x: 16.695105 ft <br />Maximum displacement in X-direction 35.230 in Member No. 5, x: 12.591175 ft <br />Maximum deformations <br />Resultant of reactions about Z -2.21 kipft At center of gravity of model <br />Resultant of reactions about Y 10.75 kipft At center of gravity of model <br />Resultant of reactions about X 9.18 kipft At center of gravity of model (8.256732, 12.812667, 7.990012 ft) <br />Resultant of reactions <br />Sum of support forces in Z -5.160 kip Deviation: 0.00 % <br />Sum of loads in Z -5.160 kip <br />Sum of support forces in Y 0.001 kip Deviation: 0.01 % <br />Sum of loads in Y 0.001 kip <br />Sum of support forces in X 1.222 kip Deviation: 0.00 % <br />Sum of loads in X 1.222 kip <br />Sum of loads and sum of support forces <br />4 CO24 - 1.20D + W1 + 0.50Lr <br />Speed of convergence 1.00 -- <br />Integrate preliminary form-finding <br />Number of iterations for loading prestress 15 <br />Plate bending theory Mindlin <br />Method for Equation System Direct <br />Try to calculate unstable structure <br />Consider favorable effects due to tension forces of members <br />Divide results by load factor <br />Multiplier factor 1.00 -- <br />Modify loading by multiplier factor <br />Number of load increments 1 <br />Maximum number of iterations 500 <br />Iterative method Newton-Raphson <br />Analysis type Large deformations <br />Static Analysis Settings No. 1 - Large deformations | Newton-Raphson | 500 | 1 <br />Infinity Norm 8.89e+09 -- <br />Stiffness matrix determinant 3.98e+6699 -- <br />Minimum value of element of stiffness matrix on diagonal 100.00 -- <br />Maximum value of element of stiffness matrix on diagonal 4.40e+09 -- <br />Number of iterations 7 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis -7.7 mrad Member No. 2, x: 18.330000 ft <br />Maximum rotation about X-axis -4.9 mrad Member No. 2, x: 18.330000 ft <br />Maximum vectorial displacement 39.295 in Member No. 8, x: 14.702599 ft <br />Maximum displacement in Z-direction -22.172 in FE node No. 327: (-2.728428, 17.790018, 15.663158 ft) <br />Maximum displacement in Y-direction 37.571 in Member No. 8, x: 14.702599 ft <br />Maximum displacement in X-direction -33.666 in Member No. 7, x: 13.033478 ft <br />Maximum deformations <br />Resultant of reactions about Z -0.70 kipft At center of gravity of model <br />Resultant of reactions about Y -15.69 kipft At center of gravity of model <br />Resultant of reactions about X -4.60 kipft At center of gravity of model (8.256732, 12.812667, 7.990012 ft) <br />Resultant of reactions <br />Sum of support forces in Z -3.180 kip Deviation: 0.00 % <br />Sum of loads in Z -3.180 kip <br />Sum of support forces in Y 1.234 kip Deviation: 0.00 % <br />Sum of loads in Y 1.234 kip <br />Sum of support forces in X -0.130 kip Deviation: 0.00 % <br />Sum of loads in X -0.130 kip <br />Description Value Unit Notes