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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 11 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis -15.9 mrad Member No. 2, x: 18.330000 ft <br />Maximum rotation about X-axis 10.3 mrad Member No. 1, x: 18.330000 ft <br />Maximum vectorial displacement 63.525 in FE node No. 211: (8.643770, 11.991210, 15.000000 ft) <br />Maximum displacement in Z-direction -63.511 in FE node No. 211: (8.643770, 11.991210, 15.000000 ft) <br />Maximum displacement in Y-direction -38.618 in Member No. 6, x: 18.212842 ft <br />Maximum displacement in X-direction 34.880 in Member No. 5, x: 12.591175 ft <br />Maximum deformations <br />Resultant of reactions about Z -1.11 kipft At center of gravity of model <br />Resultant of reactions about Y 5.54 kipft At center of gravity of model <br />Resultant of reactions about X 5.43 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 -7.621 kip Deviation: 0.00 % <br />Sum of loads in Z -7.621 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 0.611 kip Deviation: 0.00 % <br />Sum of loads in X 0.611 kip <br />Sum of loads and sum of support forces <br />3 CO7 - 1.20D + 0.50W1 + 1.60Lr <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 8.92e+09 -- <br />Stiffness matrix determinant 1.30e+6764 -- <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 9 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis 9.3 mrad Member No. 1, x: 18.330000 ft <br />Maximum rotation about X-axis 6.5 mrad Member No. 1, x: 18.330000 ft <br />Maximum vectorial displacement 46.713 in FE node No. 250: (5.079897, 13.443921, 15.031579 ft) <br />Maximum displacement in Z-direction -46.533 in FE node No. 250: (5.079897, 13.443921, 15.031579 ft) <br />Maximum displacement in Y-direction -37.167 in Member No. 6, x: 16.695105 ft <br />Maximum displacement in X-direction 31.669 in Member No. 5, x: 12.591175 ft <br />Maximum deformations <br />Resultant of reactions about Z -0.35 kipft At center of gravity of model <br />Resultant of reactions about Y -7.78 kipft At center of gravity of model <br />Resultant of reactions about X -1.76 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 -5.285 kip Deviation: 0.00 % <br />Sum of loads in Z -5.285 kip <br />Sum of support forces in Y 0.617 kip Deviation: 0.00 % <br />Sum of loads in Y 0.617 kip <br />Sum of support forces in X -0.065 kip Deviation: 0.00 % <br />Sum of loads in X -0.065 kip <br />Description Value Unit Notes