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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 8.99e+09 -- <br />Stiffness matrix determinant 1.51e+6886 -- <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 10 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis 14.8 mrad Member No. 1, x: 18.330000 ft <br />Maximum rotation about X-axis 10.1 mrad Member No. 1, x: 18.330000 ft <br />Maximum vectorial displacement 60.678 in FE node No. 210: (8.004936, 13.323567, 15.000000 ft) <br />Maximum displacement in Z-direction -60.659 in FE node No. 211: (8.643770, 11.991210, 15.000000 ft) <br />Maximum displacement in Y-direction -38.224 in Member No. 6, x: 16.695105 ft <br />Maximum displacement in X-direction 33.825 in Member No. 5, x: 12.591175 ft <br />Maximum deformations <br />Resultant of reactions about Z 0.00 kipft At center of gravity of model <br />Resultant of reactions about Y 0.20 kipft At center of gravity of model <br />Resultant of reactions about X 1.03 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 -7.427 kip Deviation: 0.00 % <br />Sum of loads in Z -7.427 kip <br />Sum of support forces in Y 0.000 kip <br />Sum of loads in Y 0.000 kip <br />Sum of support forces in X 0.000 kip <br />Sum of loads in X 0.000 kip <br />Sum of loads and sum of support forces <br />3 CO13 - 1.20D + 1.60Lr <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 8.93e+09 -- <br />Stiffness matrix determinant 4.87e+6807 -- <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 9 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis 10.5 mrad Member No. 1, x: 18.330000 ft <br />Maximum rotation about X-axis 7.2 mrad Member No. 1, x: 18.330000 ft <br />Maximum vectorial displacement 51.840 in FE node No. 210: (8.004936, 13.323567, 15.000000 ft) <br />Maximum displacement in Z-direction -51.800 in FE node No. 210: (8.004936, 13.323567, 15.000000 ft) <br />Maximum displacement in Y-direction -37.537 in Member No. 6, x: 16.695105 ft <br />Maximum displacement in X-direction 33.196 in Member No. 5, x: 12.591175 ft <br />Maximum deformations <br />Resultant of reactions about Z 0.00 kipft At center of gravity of model <br />Resultant of reactions about Y 0.12 kipft At center of gravity of model <br />Resultant of reactions about X 0.60 kipft At center of gravity of model (8.256732, 12.812667, 7.990012 ft) <br />Description Value Unit Notes