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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 8.92e+09 -- <br />Stiffness matrix determinant 1.96e+6800 -- <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. 2, x: 18.330000 ft <br />Maximum rotation about X-axis 6.6 mrad Member No. 1, x: 18.330000 ft <br />Maximum vectorial displacement 52.649 in FE node No. 211: (8.643770, 11.991210, 15.000000 ft) <br />Maximum displacement in Z-direction -52.632 in FE node No. 211: (8.643770, 11.991210, 15.000000 ft) <br />Maximum displacement in Y-direction -37.814 in Member No. 6, x: 16.695105 ft <br />Maximum displacement in X-direction 34.297 in Member No. 5, x: 12.591175 ft <br />Maximum deformations <br />Resultant of reactions about Z -1.00 kipft At center of gravity of model <br />Resultant of reactions about Y 4.91 kipft At center of gravity of model <br />Resultant of reactions about X 4.46 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 -4.962 kip Deviation: 0.00 % <br />Sum of loads in Z -4.962 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 0.550 kip Deviation: 0.00 % <br />Sum of loads in X 0.550 kip <br />Sum of loads and sum of support forces <br />6 CO47 - D + 0.45W1 + 0.75Lr <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 8.86e+09 -- <br />Stiffness matrix determinant 1.75e+6639 -- <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 5.0 mrad Member No. 1, x: 18.330000 ft <br />Maximum rotation about X-axis 3.6 mrad Member No. 1, x: 18.330000 ft <br />Maximum vectorial displacement 38.730 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in Z-direction -32.614 in FE node No. 289: (1.506747, 14.920703, 15.189474 ft) <br />Maximum displacement in Y-direction -36.537 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in X-direction -31.071 in Member No. 7, x: 13.033478 ft <br />Maximum deformations <br />Resultant of reactions about Z -0.32 kipft At center of gravity of model <br />Resultant of reactions about Y -7.06 kipft At center of gravity of model <br />Resultant of reactions about X -1.88 kipft At center of gravity of model (8.256732, 12.812667, 7.990012 ft) <br />Description Value Unit Notes