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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 5.71e+13 -- <br />Number of iterations 12 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad Member No. 4, x: 19.548077 ft <br />Maximum rotation about Y-axis 11.6 mrad Member No. 2, x: 19.330000 ft <br />Maximum rotation about X-axis -13.6 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 73.249 in FE node No. 620: (14.075309, -15.826300, 15.240000 ft) <br />Maximum displacement in Z-direction -73.118 in FE node No. 619: (12.605900, -15.952613, 15.273333 ft) <br />Maximum displacement in Y-direction 51.295 in Member No. 11, x: 18.189018 ft <br />Maximum displacement in X-direction -52.078 in Member No. 13, x: 20.689090 ft <br />Maximum deformations <br />Resultant of reactions about Z 3.77 kipft At center of gravity of model <br />Resultant of reactions about Y 24.21 kipft At center of gravity of model <br />Resultant of reactions about X 38.31 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 -13.668 kip Deviation: 0.00 % <br />Sum of loads in Z -13.668 kip <br />Sum of support forces in Y -1.204 kip Deviation: 0.00 % <br />Sum of loads in Y -1.204 kip <br />Sum of support forces in X -0.267 kip Deviation: 0.00 % <br />Sum of loads in X -0.267 kip <br />Sum of loads and sum of support forces <br />3 CO8 - 1.20D + 0.50W2 + 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 1.27e+14 -- <br />Stiffness matrix determinant 7.53e+14069 -- <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 13 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.1 mrad Member No. 1, x: 0.000000 ft <br />Maximum rotation about Y-axis 11.9 mrad Member No. 5, x: 13.330000 ft <br />Maximum rotation about X-axis -15.6 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 71.948 in FE node No. 596: (15.682394, -14.256809, 15.251667 ft) <br />Maximum displacement in Z-direction -71.795 in FE node No. 596: (15.682394, -14.256809, 15.251667 ft) <br />Maximum displacement in Y-direction 52.015 in Member No. 11, x: 18.189018 ft <br />Maximum displacement in X-direction -50.668 in Member No. 13, x: 20.689090 ft <br />Maximum deformations <br />Resultant of reactions about Z -4.09 kipft At center of gravity of model <br />Resultant of reactions about Y 0.04 kipft At center of gravity of model <br />Resultant of reactions about X 18.81 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 -15.412 kip Deviation: 0.00 % <br />Sum of loads in Z -15.412 kip <br />Sum of support forces in Y 0.207 kip Deviation: 0.00 % <br />Sum of loads in Y 0.207 kip <br />Sum of support forces in X 1.463 kip Deviation: 0.00 % <br />Sum of loads in X 1.463 kip <br />Description Value Unit Notes