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Infinity Norm 1.27e+14 -- <br />Stiffness matrix determinant 4.58e+14118 -- <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 11.4 mrad Member No. 2, x: 19.330000 ft <br />Maximum rotation about X-axis -16.5 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 70.391 in FE node No. 646: (15.407042, -17.143167, 15.161667 ft) <br />Maximum displacement in Z-direction 70.163 in FE node No. 646: (15.407042, -17.143167, 15.161667 ft) <br />Maximum displacement in Y-direction 52.297 in Member No. 11, x: 21.496112 ft <br />Maximum displacement in X-direction -52.691 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 -30.28 kipft At center of gravity of model <br />Resultant of reactions about X -41.55 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 12.032 kip Deviation: 0.00 % <br />Sum of loads in Z 12.032 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 />W LC9 - Uplift <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 2.66e+13661 -- <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 11 <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 7.7 mrad Member No. 5, x: 13.330000 ft <br />Maximum rotation about X-axis 7.0 mrad Member No. 4, x: 20.330000 ft <br />Maximum vectorial displacement 52.203 in Member No. 13, x: 17.506153 ft <br />Maximum displacement in Z-direction 34.108 in FE node No. 150: (-15.734906, -9.004946, 15.954681 ft) <br />Maximum displacement in Y-direction 48.183 in Member No. 11, x: 19.842565 ft <br />Maximum displacement in X-direction -49.759 in Member No. 13, x: 17.506153 ft <br />Maximum deformations <br />Resultant of reactions about Z 7.65 kipft At center of gravity of model <br />Resultant of reactions about Y -0.11 kipft At center of gravity of model <br />Resultant of reactions about X 14.87 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 3.284 kip Deviation: 0.00 % <br />Sum of loads in Z 3.284 kip <br />Sum of support forces in Y -2.409 kip Deviation: 0.00 % <br />Description Value Unit Notes