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Number of iterations 5 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis -1.1 mrad Member No. 2, x: 18.330000 ft <br />Maximum rotation about X-axis 0.8 mrad Member No. 1, x: 18.330000 ft <br />Maximum vectorial displacement 36.445 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in Z-direction -13.434 in FE node No. 210: (8.004936, 13.323567, 15.000000 ft) <br />Maximum displacement in Y-direction -36.221 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in X-direction 32.412 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 0.01 kipft At center of gravity of model <br />Resultant of reactions about X 0.00 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 -2.931 kip Deviation: 0.00 % <br />Sum of loads in Z -2.931 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 />D LC2 - Dead Load <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 8.81e+09 -- <br />Stiffness matrix determinant 5.22e+8837 -- <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 34 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis 1.0 mrad Member No. 1, x: 18.330000 ft <br />Maximum rotation about X-axis 0.7 mrad Member No. 1, x: 18.330000 ft <br />Maximum vectorial displacement 36.533 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in Z-direction -10.951 in FE node No. 210: (8.004936, 13.323567, 15.000000 ft) <br />Maximum displacement in Y-direction -36.459 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in X-direction 32.778 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 0.00 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 0.000 kip <br />Sum of loads in Z 0.000 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 />Tp LC1 - Prestress <br />Description Value Unit Notes