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Maximum displacement in Z-direction -64.085 in FE node No. 620: (14.075309, -15.826300, 15.240000 ft) <br />Maximum displacement in Y-direction 50.946 in Member No. 11, x: 18.189018 ft <br />Maximum displacement in X-direction -50.786 in Member No. 13, x: 20.689090 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 15.12 kipft At center of gravity of model <br />Resultant of reactions about X 19.42 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 -10.880 kip Deviation: 0.00 % <br />Sum of loads in Z -10.880 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 />3 CO36 - D + Lr <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 8.51e+13750 -- <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 0.0 mrad Member No. 1, x: 0.000000 ft <br />Maximum rotation about Y-axis 6.1 mrad Member No. 2, x: 19.330000 ft <br />Maximum rotation about X-axis -8.0 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 53.437 in FE node No. 620: (14.075309, -15.826300, 15.240000 ft) <br />Maximum displacement in Z-direction -53.248 in FE node No. 620: (14.075309, -15.826300, 15.240000 ft) <br />Maximum displacement in Y-direction 50.066 in Member No. 11, x: 18.189018 ft <br />Maximum displacement in X-direction -49.908 in Member No. 13, x: 20.689090 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 8.82 kipft At center of gravity of model <br />Resultant of reactions about X 11.28 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 -8.467 kip Deviation: 0.00 % <br />Sum of loads in Z -8.467 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 />3 CO35 - D + S <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 />Description Value Unit Notes