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Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis -5.4 mrad Member No. 2, x: 18.330000 ft <br />Maximum rotation about X-axis -3.4 mrad Member No. 2, x: 18.330000 ft <br />Maximum vectorial displacement 38.182 in Member No. 6, x: 16.695105 ft <br />Maximum displacement in Z-direction -35.019 in FE node No. 249: (4.436425, 14.788313, 15.094737 ft) <br />Maximum displacement in Y-direction 37.133 in Member No. 8, x: 14.702599 ft <br />Maximum displacement in X-direction 32.603 in Member No. 5, x: 14.165072 ft <br />Maximum deformations <br />Resultant of reactions about Z -0.48 kipft At center of gravity of model <br />Resultant of reactions about Y -6.44 kipft At center of gravity of model <br />Resultant of reactions about X -4.86 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 -2.022 kip Deviation: 0.00 % <br />Sum of loads in Z -2.022 kip <br />Sum of support forces in Y 0.020 kip Deviation: 0.00 % <br />Sum of loads in Y 0.020 kip <br />Sum of support forces in X -0.735 kip Deviation: 0.00 % <br />Sum of loads in X -0.735 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 />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 8.92e+09 -- <br />Stiffness matrix determinant 6.19e+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 10 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis 9.8 mrad FE node No. 4: (-12.578492, 26.458141, 18.000000 ft) <br />Maximum rotation about X-axis -8.0 mrad Member No. 3, x: 12.330000 ft <br />Maximum vectorial displacement 42.505 in Member No. 6, x: 16.695105 ft <br />Maximum displacement in Z-direction 30.889 in FE node No. 231: (7.183570, 12.045370, 14.984211 ft) <br />Maximum displacement in Y-direction -39.479 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in X-direction 37.045 in Member No. 5, x: 14.165072 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 -0.14 kipft At center of gravity of model <br />Resultant of reactions about X -0.81 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 1.324 kip Deviation: 0.00 % <br />Sum of loads in Z 1.324 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 />7 CO54 - 0.60D + 0.60W3 <br />Speed of convergence 1.00 -- <br />Integrate preliminary form-finding <br />Description Value Unit Notes