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Maximum rotation about Z-axis 0.0 mrad Member No. 1, x: 0.000000 ft <br />Maximum rotation about Y-axis 7.4 mrad Member No. 5, x: 13.330000 ft <br />Maximum rotation about X-axis -8.9 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 51.143 in Member No. 11, x: 16.535471 ft <br />Maximum displacement in Z-direction -37.325 in FE node No. 718: (10.435596, -21.725328, 15.426667 ft) <br />Maximum displacement in Y-direction 48.212 in Member No. 11, x: 16.535471 ft <br />Maximum displacement in X-direction -48.764 in Member No. 13, x: 20.689090 ft <br />Maximum deformations <br />Resultant of reactions about Z 1.15 kipft At center of gravity of model <br />Resultant of reactions about Y 26.88 kipft At center of gravity of model <br />Resultant of reactions about X 20.62 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 -4.705 kip Deviation: 0.00 % <br />Sum of loads in Z -4.705 kip <br />Sum of support forces in Y -0.368 kip Deviation: 0.00 % <br />Sum of loads in Y -0.368 kip <br />Sum of support forces in X -2.901 kip Deviation: 0.00 % <br />Sum of loads in X -2.901 kip <br />Sum of loads and sum of support forces <br />4 CO22 - 1.20D + W4 + 0.50S <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 2.74e+14061 -- <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 13 <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 10.1 mrad Member No. 2, x: 19.330000 ft <br />Maximum rotation about X-axis -14.8 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 65.964 in FE node No. 646: (15.407042, -17.143167, 15.161667 ft) <br />Maximum displacement in Z-direction 65.718 in FE node No. 646: (15.407042, -17.143167, 15.161667 ft) <br />Maximum displacement in Y-direction 51.987 in Member No. 11, x: 21.496112 ft <br />Maximum displacement in X-direction -52.371 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 -26.16 kipft At center of gravity of model <br />Resultant of reactions about X -36.07 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 4.276 kip Deviation: 0.00 % <br />Sum of loads in Z 4.276 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 />4 CO21 - 1.20D + W3 + 0.50S <br />Speed of convergence 1.00 -- <br />Integrate preliminary form-finding <br />Description Value Unit Notes