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Static Analysis Settings No. 1 - Large deformations | Newton-Raphson | 500 | 1 <br />Infinity Norm 1.27e+14 -- <br />Stiffness matrix determinant 2.21e+13655 -- <br />Minimum value of element of stiffness matrix on diagonal 100.00 -- <br />Maximum value of element of stiffness matrix on diagonal 5.71e+13 -- <br />Number of iterations 10 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad Member No. 2, x: 18.256111 ft <br />Maximum rotation about Y-axis 5.0 mrad Member No. 2, x: 19.330000 ft <br />Maximum rotation about X-axis -6.7 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 52.063 in Member No. 11, x: 18.189018 ft <br />Maximum displacement in Z-direction -46.579 in FE node No. 669: (12.280485, -18.796866, 15.283333 ft) <br />Maximum displacement in Y-direction 48.749 in Member No. 11, x: 18.189018 ft <br />Maximum displacement in X-direction -49.981 in Member No. 13, x: 22.280559 ft <br />Maximum deformations <br />Resultant of reactions about Z 0.54 kipft At center of gravity of model <br />Resultant of reactions about Y 16.83 kipft At center of gravity of model <br />Resultant of reactions about X 15.35 kipft At center of gravity of model (5.206824, -11.262029, 8.906877 ft) <br />Resultant of reactions <br />Sum of support forces in Z -6.229 kip Deviation: 0.00 % <br />Sum of loads in Z -6.229 kip <br />Sum of support forces in Y -0.166 kip Deviation: 0.00 % <br />Sum of loads in Y -0.166 kip <br />Sum of support forces in X -1.305 kip Deviation: 0.00 % <br />Sum of loads in X -1.305 kip <br />Sum of loads and sum of support forces <br />6 CO45 - D + 0.45W4 + 0.75S <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 1.27e+14 -- <br />Stiffness matrix determinant 9.49e+13626 -- <br />Minimum value of element of stiffness matrix on diagonal 100.00 -- <br />Maximum value of element of stiffness matrix on diagonal 5.71e+13 -- <br />Number of iterations 9 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad Member No. 1, x: 0.000000 ft <br />Maximum rotation about Y-axis 4.0 mrad Member No. 5, x: 13.330000 ft <br />Maximum rotation about X-axis -6.2 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 52.369 in Member No. 13, x: 19.097622 ft <br />Maximum displacement in Z-direction 37.031 in FE node No. 672: (16.763808, -18.481086, 15.033333 ft) <br />Maximum displacement in Y-direction 49.839 in Member No. 11, x: 21.496112 ft <br />Maximum displacement in X-direction -50.106 in Member No. 13, x: 19.097622 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 -7.52 kipft At center of gravity of model <br />Resultant of reactions about X -10.45 kipft At center of gravity of model (5.206824, -11.262029, 8.906877 ft) <br />Resultant of reactions <br />Sum of support forces in Z -2.126 kip Deviation: 0.00 % <br />Sum of loads in Z -2.126 kip <br />Description Value Unit Notes