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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 />W LC8 - Wind @ 90 Deg. <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 6.10e+13794 -- <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 11 <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 10.4 mrad Member No. 5, x: 13.330000 ft <br />Maximum rotation about X-axis -12.9 mrad Member No. 2, x: 19.330000 ft <br />Maximum vectorial displacement 54.182 in Member No. 11, x: 21.496112 ft <br />Maximum displacement in Z-direction -39.279 in FE node No. 162: (-14.195496, -13.507419, 15.762452 ft) <br />Maximum displacement in Y-direction 51.452 in Member No. 11, x: 21.496112 ft <br />Maximum displacement in X-direction -50.293 in Member No. 13, x: 20.689090 ft <br />Maximum deformations <br />Resultant of reactions about Z -8.30 kipft At center of gravity of model <br />Resultant of reactions about Y -48.52 kipft At center of gravity of model <br />Resultant of reactions about X -23.77 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 -0.226 kip Deviation: 0.00 % <br />Sum of loads in Z -0.226 kip <br />Sum of support forces in Y 0.415 kip Deviation: 0.00 % <br />Sum of loads in Y 0.415 kip <br />Sum of support forces in X 2.927 kip Deviation: 0.00 % <br />Sum of loads in X 2.927 kip <br />Sum of loads and sum of support forces <br />W LC6 - Wind @ 0 Deg. <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 3.67e+13739 -- <br />Minimum value of element of stiffness matrix on diagonal 100.00 -- <br />Description Value Unit Notes