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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 7.06e+13629 -- <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 9 <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 6.5 mrad Member No. 5, x: 13.330000 ft <br />Maximum rotation about X-axis -6.3 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 50.769 in FE node No. 582: (31.708218, -11.192625, 15.480000 ft) <br />Maximum displacement in Z-direction 31.093 in FE node No. 137: (-17.182116, -9.004946, 15.673076 ft) <br />Maximum displacement in Y-direction 47.309 in Member No. 11, x: 19.842565 ft <br />Maximum displacement in X-direction -50.208 in Member No. 13, x: 17.506153 ft <br />Maximum deformations <br />Resultant of reactions about Z 7.68 kipft At center of gravity of model <br />Resultant of reactions about Y 4.28 kipft At center of gravity of model <br />Resultant of reactions about X 20.50 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 -4.519 kip Deviation: 0.00 % <br />Sum of loads in Z -4.519 kip <br />Sum of support forces in Y -2.409 kip Deviation: 0.00 % <br />Sum of loads in Y -2.409 kip <br />Sum of support forces in X -0.534 kip Deviation: 0.00 % <br />Sum of loads in X -0.534 kip <br />Sum of loads and sum of support forces <br />4 CO20 - 1.20D + W2 + 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 1.27e+14 -- <br />Stiffness matrix determinant 8.64e+13760 -- <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 10 <br />Calculation statistic <br />Maximum rotation about Z-axis -0.1 mrad Member No. 4, x: 19.313500 ft <br />Maximum rotation about Y-axis 11.3 mrad Member No. 5, x: 13.330000 ft <br />Maximum rotation about X-axis -12.8 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 53.573 in Member No. 9, x: 19.155968 ft <br />Description Value Unit Notes