Laserfiche WebLink
Maximum displacement in Z-direction -34.383 in FE node No. 172: (12.198367, 10.562570, 15.094737 ft) <br />Maximum displacement in Y-direction -38.295 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in X-direction 34.494 in Member No. 5, x: 14.165072 ft <br />Maximum deformations <br />Resultant of reactions about Z -1.33 kipft At center of gravity of model <br />Resultant of reactions about Y 6.38 kipft At center of gravity of model <br />Resultant of reactions about X 5.28 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 -2.010 kip Deviation: 0.00 % <br />Sum of loads in Z -2.010 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 0.733 kip Deviation: 0.00 % <br />Sum of loads in X 0.733 kip <br />Sum of loads and sum of support forces <br />7 CO52 - 0.60D + 0.60W1 <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 8.90e+09 -- <br />Stiffness matrix determinant 1.20e+6729 -- <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 7.9 mrad Member No. 1, x: 18.330000 ft <br />Maximum rotation about X-axis 5.5 mrad Member No. 1, x: 18.330000 ft <br />Maximum vectorial displacement 43.135 in FE node No. 270: (3.617378, 13.504098, 15.047368 ft) <br />Maximum displacement in Z-direction -42.931 in FE node No. 250: (5.079897, 13.443921, 15.031579 ft) <br />Maximum displacement in Y-direction -36.943 in Member No. 6, x: 15.177368 ft <br />Maximum displacement in X-direction 31.454 in FE node No. 412: (-5.296207, 11.140270, 14.526316 ft) <br />Maximum deformations <br />Resultant of reactions about Z -0.31 kipft At center of gravity of model <br />Resultant of reactions about Y -7.02 kipft At center of gravity of model <br />Resultant of reactions about X -1.65 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 -4.316 kip Deviation: 0.00 % <br />Sum of loads in Z -4.316 kip <br />Sum of support forces in Y 0.555 kip Deviation: 0.00 % <br />Sum of loads in Y 0.555 kip <br />Sum of support forces in X -0.059 kip Deviation: 0.00 % <br />Sum of loads in X -0.059 kip <br />Sum of loads and sum of support forces <br />6 CO51 - D + 0.45W5 + 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 />Description Value Unit Notes