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Sum of loads and sum of support forces <br />4 CO24 - 1.20D + W1 + 0.50Lr <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 1.20e+13774 -- <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 7.9 mrad Member No. 5, x: 13.330000 ft <br />Maximum rotation about X-axis -9.6 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 52.164 in Member No. 13, x: 22.280559 ft <br />Maximum displacement in Z-direction -43.999 in FE node No. 574: (20.153201, -12.371538, 15.346667 ft) <br />Maximum displacement in Y-direction 49.250 in Member No. 11, x: 16.535471 ft <br />Maximum displacement in X-direction -48.152 in Member No. 13, x: 22.280559 ft <br />Maximum deformations <br />Resultant of reactions about Z -2.14 kipft At center of gravity of model <br />Resultant of reactions about Y 5.43 kipft At center of gravity of model <br />Resultant of reactions about X 3.64 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 -9.552 kip Deviation: 0.00 % <br />Sum of loads in Z -9.552 kip <br />Sum of support forces in Y 2.336 kip Deviation: 0.00 % <br />Sum of loads in Y 2.336 kip <br />Sum of support forces in X 0.552 kip Deviation: 0.00 % <br />Sum of loads in X 0.552 kip <br />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 1.27e+14 -- <br />Stiffness matrix determinant 1.49e+13731 -- <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 />Description Value Unit Notes