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0.60 W LC11 W A2 <br />0.60 D LC2 D A1 <br />56 7 0.60D + 0.60W5 <br />0.60 W LC10 W A2 <br />0.60 D LC2 D A1 <br />55 7 0.60D + 0.60W4 <br />0.60 W LC9 W A2 <br />0.60 D LC2 D A1 <br />54 7 0.60D + 0.60W3 <br />No.Factor Load Case Action <br />CO <br />Stability check based on deformation rate <br />Equilibrium for undeformed structure <br />Speed of convergence 1.00 -- <br />Number of iterations for loading prestress 15 <br />Activate mass conversion to load <br />Plate bending theory Mindlin <br />Method for equation system Direct <br />pressure' (Bourdon effect) <br />Displacements due to member load of type 'Pipe internal <br />Try to calculate unstable structure <br />Consider favorable effect due to tension in members <br />Divide results by load factor <br />Loading multiplier factor k 1.00 -- <br />Modify loading by multiplier factor <br />Integrate preliminary form-finding <br />Ignore all nonlinearities <br />Modify standard precision and tolerance settings <br />Number of load increments 1 <br />Maximum number of iterations 500 <br />Iterative method for nonlinear analysis Newton-Raphson <br />Analysis type Large deformations <br />1 Large deformations | Newton-Raphson | 500 | 1 <br />No.Description Symbol Value Unit <br />Settings <br />Specific turbulent dissipation rate ω 0.500 -- <br />Turbulent dissipation rate ε 0.500 -- <br />Turbulent kinetic energy k 0.500 -- <br />Velocity field U 0.500 -- <br />Pressure field P 0.200 -- <br />Residual pressure P 0.010 -- <br />Residual type Pressure <br />Turbulence model type RANS k-ε <br />Minimum number of iterations 300 <br />Maximum number of iterations 500 <br />Use second-order numerical scheme <br />Use potential flow solver to calculate initial condition <br />Boundary layers checked <br />Snap to model edges <br />Mesh refinement type Distance from Surface <br />Finite volume mesh density 20.00 % <br />Numerical solver OpenFOAM <br />Member load distribution Concentrated <br />Save solver data to continue calculation <br />User-defined dimensions of wind tunnel <br />Consider surface roughness <br />'Slip' boundary condition on bottom boundary <br />Consider turbulence... <br />Kinematic viscosity ν 0.000161 ft2/s <br />Simulation type Steady Flow <br />1 <br />No.Description Symbol Value Unit <br />Settings