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Maximum rotation about Z-axis 0.0 mrad Member No. 4, x: 19.313500 ft <br />Maximum rotation about Y-axis 8.7 mrad FE node No. 5: (-7.162202, -33.018136, 19.000000 ft) <br />Maximum rotation about X-axis -9.3 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 61.754 in FE node No. 645: (13.925117, -17.258953, 15.220000 ft) <br />Maximum displacement in Z-direction -61.520 in FE node No. 644: (12.443192, -17.374739, 15.278333 ft) <br />Maximum displacement in Y-direction 50.044 in Member No. 11, x: 18.189018 ft <br />Maximum displacement in X-direction -51.237 in Member No. 13, x: 22.280559 ft <br />Maximum deformations <br />Resultant of reactions about Z 0.64 kipft At center of gravity of model <br />Resultant of reactions about Y 25.88 kipft At center of gravity of model <br />Resultant of reactions about X 25.65 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 -9.910 kip Deviation: 0.00 % <br />Sum of loads in Z -9.910 kip <br />Sum of support forces in Y -0.184 kip Deviation: 0.00 % <br />Sum of loads in Y -0.184 kip <br />Sum of support forces in X -1.450 kip Deviation: 0.00 % <br />Sum of loads in X -1.450 kip <br />Sum of loads and sum of support forces <br />3 CO5 - 1.20D + 0.50W4 + 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 1.27e+14 -- <br />Stiffness matrix determinant 1.01e+13153 -- <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 7 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis 1.5 mrad Member No. 5, x: 13.330000 ft <br />Maximum rotation about X-axis -2.2 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 48.966 in Member No. 13, x: 19.097622 ft <br />Maximum displacement in Z-direction 15.804 in Member No. 9, x: 19.155968 ft <br />Maximum displacement in Y-direction 48.302 in Member No. 11, x: 19.842565 ft <br />Maximum displacement in X-direction -48.539 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 -1.79 kipft At center of gravity of model <br />Resultant of reactions about X -2.71 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 -5.398 kip Deviation: 0.00 % <br />Sum of loads in Z -5.398 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 />Description Value Unit Notes