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Sum of loads and sum of support forces <br />4 CO23 - 1.20D + W5 + 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 8.91e+09 -- <br />Stiffness matrix determinant 3.62e+6768 -- <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 8.8 mrad Member No. 1, x: 18.330000 ft <br />Maximum rotation about X-axis 6.1 mrad Member No. 1, x: 18.330000 ft <br />Maximum vectorial displacement 48.914 in FE node No. 229: (5.901263, 14.722119, 15.047368 ft) <br />Maximum displacement in Z-direction -48.752 in FE node No. 229: (5.901263, 14.722119, 15.047368 ft) <br />Maximum displacement in Y-direction 37.471 in Member No. 8, x: 16.172859 ft <br />Maximum displacement in X-direction 32.918 in Member No. 5, x: 14.165072 ft <br />Maximum deformations <br />Resultant of reactions about Z -0.80 kipft At center of gravity of model <br />Resultant of reactions about Y -10.73 kipft At center of gravity of model <br />Resultant of reactions about X -7.96 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 -4.667 kip Deviation: 0.00 % <br />Sum of loads in Z -4.667 kip <br />Sum of support forces in Y 0.033 kip Deviation: 0.00 % <br />Sum of loads in Y 0.033 kip <br />Sum of support forces in X -1.225 kip Deviation: 0.00 % <br />Sum of loads in X -1.225 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 8.96e+09 -- <br />Stiffness matrix determinant 1.01e+6863 -- <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 10 <br />Calculation statistic <br />Description Value Unit Notes