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Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis 1.7 mrad Member No. 1, x: 18.330000 ft <br />Maximum rotation about X-axis -1.5 mrad Member No. 3, x: 12.330000 ft <br />Maximum vectorial displacement 37.427 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in Z-direction 3.971 in Member No. 5, x: 12.591175 ft <br />Maximum displacement in Y-direction -37.217 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in X-direction 33.792 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 0.00 kipft At center of gravity of model <br />Resultant of reactions about X -0.08 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 -3.213 kip Deviation: 0.00 % <br />Sum of loads in Z -3.213 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 CO4 - 1.20D + 0.50W3 + 1.60S <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 8.91e+09 -- <br />Stiffness matrix determinant 2.15e+6770 -- <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 -9.5 mrad Member No. 2, x: 18.330000 ft <br />Maximum rotation about X-axis -6.0 mrad Member No. 2, x: 18.330000 ft <br />Maximum vectorial displacement 46.884 in FE node No. 171: (11.564171, 11.882892, 15.031579 ft) <br />Maximum displacement in Z-direction -46.870 in FE node No. 191: (10.103971, 11.937051, 15.015789 ft) <br />Maximum displacement in Y-direction -37.193 in Member No. 6, x: 16.695105 ft <br />Maximum displacement in X-direction 33.348 in Member No. 5, x: 12.591175 ft <br />Maximum deformations <br />Resultant of reactions about Z -0.45 kipft At center of gravity of model <br />Resultant of reactions about Y 7.62 kipft At center of gravity of model <br />Resultant of reactions about X 2.35 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 -5.372 kip Deviation: 0.00 % <br />Sum of loads in Z -5.372 kip <br />Sum of support forces in Y -0.611 kip Deviation: 0.00 % <br />Sum of loads in Y -0.611 kip <br />Sum of support forces in X 0.093 kip Deviation: 0.00 % <br />Sum of loads in X 0.093 kip <br />Sum of loads and sum of support forces <br />3 CO3 - 1.20D + 0.50W2 + 1.60S <br />Speed of convergence 1.00 -- <br />Description Value Unit Notes