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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 8.98e+09 -- <br />Stiffness matrix determinant 3.00e+6886 -- <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 11 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis 14.0 mrad Member No. 1, x: 18.330000 ft <br />Maximum rotation about X-axis -11.1 mrad Member No. 3, x: 12.330000 ft <br />Maximum vectorial displacement 44.826 in Member No. 6, x: 16.695105 ft <br />Maximum displacement in Z-direction 40.701 in FE node No. 231: (7.183570, 12.045370, 14.984211 ft) <br />Maximum displacement in Y-direction -40.298 in Member No. 6, x: 16.695105 ft <br />Maximum displacement in X-direction 38.239 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 -0.24 kipft At center of gravity of model <br />Resultant of reactions about X -1.34 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 1.571 kip Deviation: 0.00 % <br />Sum of loads in Z 1.571 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 CO16 - 1.20D + W3 <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 8.90e+09 -- <br />Stiffness matrix determinant 1.48e+6708 -- <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 8 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis 8.1 mrad Member No. 1, x: 18.330000 ft <br />Maximum rotation about X-axis 5.7 mrad Member No. 1, x: 18.330000 ft <br />Maximum vectorial displacement 41.420 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in Z-direction 18.546 in FE node No. 264: (-0.257372, 21.606557, 15.615789 ft) <br />Maximum displacement in Y-direction -38.916 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in X-direction 36.577 in Member No. 5, x: 14.165072 ft <br />Maximum deformations <br />Description Value Unit Notes