Laserfiche WebLink
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 8.93e+09 -- <br />Stiffness matrix determinant 2.90e+6801 -- <br />Minimum value of element of stiffness matrix on diagonal 100.00 -- <br />Maximum value of element of stiffness matrix on diagonal 4.40e+09 -- <br />Number of iterations 9 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis 10.5 mrad Member No. 1, x: 18.330000 ft <br />Maximum rotation about X-axis 7.2 mrad Member No. 1, x: 18.330000 ft <br />Maximum vectorial displacement 52.828 in FE node No. 230: (6.542417, 13.383744, 15.015789 ft) <br />Maximum displacement in Z-direction -52.760 in FE node No. 230: (6.542417, 13.383744, 15.015789 ft) <br />Maximum displacement in Y-direction -37.274 in Member No. 6, x: 16.695105 ft <br />Maximum displacement in X-direction 33.128 in Member No. 5, x: 12.591175 ft <br />Maximum deformations <br />Resultant of reactions about Z -0.36 kipft At center of gravity of model <br />Resultant of reactions about Y -4.77 kipft At center of gravity of model <br />Resultant of reactions about X -3.18 kipft At center of gravity of model (8.256732, 12.812667, 7.990012 ft) <br />Resultant of reactions <br />Sum of support forces in Z -4.971 kip Deviation: 0.00 % <br />Sum of loads in Z -4.971 kip <br />Sum of support forces in Y 0.015 kip Deviation: 0.00 % <br />Sum of loads in Y 0.015 kip <br />Sum of support forces in X -0.551 kip Deviation: 0.00 % <br />Sum of loads in X -0.551 kip <br />Sum of loads and sum of support forces <br />6 CO50 - D + 0.45W4 + 0.75Lr <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 8.83e+09 -- <br />Stiffness matrix determinant 4.95e+6536 -- <br />Minimum value of element of stiffness matrix on diagonal 100.00 -- <br />Maximum value of element of stiffness matrix on diagonal 4.40e+09 -- <br />Number of iterations 7 <br />Calculation statistic <br />Maximum rotation about Z-axis 0.0 mrad <br />Maximum rotation about Y-axis 2.5 mrad Member No. 1, x: 18.330000 ft <br />Maximum rotation about X-axis -2.1 mrad Member No. 3, x: 12.330000 ft <br />Maximum vectorial displacement 38.013 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in Z-direction 5.998 in FE node No. 412: (-5.296207, 11.140270, 14.526316 ft) <br />Maximum displacement in Y-direction -37.559 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in X-direction 34.275 in Member No. 5, x: 14.165072 ft <br />Maximum deformations <br />Description Value Unit Notes