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Maximum rotation about Z-axis 0.0 mrad Member No. 4, x: 19.548077 ft <br />Maximum rotation about Y-axis 4.9 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 49.545 in Member No. 13, x: 22.280559 ft <br />Maximum displacement in Z-direction -25.724 in FE node No. 195: (-11.301076, -13.507419, 16.325661 ft) <br />Maximum displacement in Y-direction 48.382 in Member No. 11, x: 19.842565 ft <br />Maximum displacement in X-direction -48.072 in Member No. 13, x: 22.280559 ft <br />Maximum deformations <br />Resultant of reactions about Z -1.31 kipft At center of gravity of model <br />Resultant of reactions about Y 0.53 kipft At center of gravity of model <br />Resultant of reactions about X -1.19 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 -4.112 kip Deviation: 0.00 % <br />Sum of loads in Z -4.112 kip <br />Sum of support forces in Y 1.401 kip Deviation: 0.00 % <br />Sum of loads in Y 1.401 kip <br />Sum of support forces in X 0.331 kip Deviation: 0.00 % <br />Sum of loads in X 0.331 kip <br />Sum of loads and sum of support forces <br />7 CO56 - 0.60D + 0.60W5 <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 4.24e+13515 -- <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 8 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.1 mrad Member No. 1, x: 0.000000 ft <br />Maximum rotation about Y-axis 6.2 mrad Member No. 5, x: 13.330000 ft <br />Maximum rotation about X-axis 6.4 mrad Member No. 4, x: 20.330000 ft <br />Maximum vectorial displacement 49.389 in Member No. 9, x: 20.629504 ft <br />Maximum displacement in Z-direction 31.511 in FE node No. 211: (-9.701261, -16.500830, 16.310011 ft) <br />Maximum displacement in Y-direction 48.235 in Member No. 11, x: 16.535471 ft <br />Maximum displacement in X-direction -48.430 in Member No. 13, x: 17.506153 ft <br />Maximum deformations <br />Resultant of reactions about Z 0.73 kipft At center of gravity of model <br />Resultant of reactions about Y 13.62 kipft At center of gravity of model <br />Resultant of reactions about X 8.92 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 -1.205 kip Deviation: 0.00 % <br />Sum of loads in Z -1.205 kip <br />Sum of support forces in Y -0.221 kip Deviation: 0.00 % <br />Sum of loads in Y -0.221 kip <br />Sum of support forces in X -1.741 kip Deviation: 0.00 % <br />Sum of loads in X -1.741 kip <br />Sum of loads and sum of support forces <br />7 CO55 - 0.60D + 0.60W4 <br />Speed of convergence 1.00 -- <br />Integrate preliminary form-finding <br />Description Value Unit Notes