Simulation of RF HEat Test

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Transcription:

Simulation of RF HEat Test Date: Tuesday, December 22, 2015 Designer: Solidworks Study name: Stress One Third Emissivity Analysis type: Nonlinear - Dynamic Description No Data Table of Contents Description... 1 Assumptions... 2 Model Information... 2 Study Properties... 3 Units... 3 Material Properties... 4 Loads and Fixtures... 5 Connector Definitions... 6 Contact Information... 6 Mesh information... 7 Sensor Details... 8 Resultant Forces... 8 Beams... 9 Study Results... 10 Conclusion... 12 Analyzed with SOLIDWORKS Simulation Simulation of RF HEat Test 1

Assumptions Model Information Solid Bodies Document Name and Reference Cut-Extrude1 Treated As Solid Body Model name: RF HEat Test Current Configuration: Default Volumetric Properties Mass:0.00361325 kg Volume:4.49968e-007 m^3 Density:8030 kg/m^3 Weight:0.0354098 N Document Path/Date Modified C:\Work\David\RF Load for ITER\RF HEat Test.SLDPRT Dec 22 08:35:19 2015 Analyzed with SOLIDWORKS Simulation Simulation of RF HEat Test 2

Study Properties Study name Analysis type Mesh type Start time End time Time increment Large displacement formulation: Update load direction with deflection: Large strain formulation: Save data for restarting the analysis Thermal Effect: Thermal option Stress One Third Emissivity Nonlinear - Dynamic Solid Mesh 0 Seconds 450 Seconds 0.03 Seconds On Off Off Off On From thermal study Input thermal study: Copy of [Trans Heat 11550000 Time Step Time 0.01 Zero strain temperature Solver type Incompatible bonding options Control technique: Iterative technique: Integration Method Result folder 4.94066e-324 298 Kelvin Direct sparse solver Simplified Force NR(Newton-Raphson) Newmark SOLIDWORKS document (C:\Work\David\RF Load for ITER) Units Unit system: Length/Displacement Temperature Angular velocity Pressure/Stress SI (MKS) mm Celsius Rad/sec N/m^2 Analyzed with SOLIDWORKS Simulation Simulation of RF HEat Test 3

Material Properties Model Reference Properties Components Curve Data:N/A Name: 304L SST Model type: Linear Elastic Isotropic Default failure Unknown criterion: Yield strength: 2.06807e+008 N/m^2 Tensile strength: 5.17017e+008 N/m^2 Elastic modulus: 1.9e+011 N/m^2 Poisson's ratio: 0.29 Mass density: 8030 kg/m^3 Shear modulus: 7.5e+010 N/m^2 Thermal expansion 1.8e-005 /Kelvin coefficient: SolidBody 1(Cut-Extrude1)(RF HEat Test) Analyzed with SOLIDWORKS Simulation Simulation of RF HEat Test 4

Loads and Fixtures Fixture name Fixture Image Fixture Details Reference Geometry-1 Entities: 1 face(s) Reference: Edge< 1 > Type: Use reference geometry Translation: ---, ---, 0 Units: mm Resultant Forces Components X Y Z Resultant Reaction force(n) -1.13715 0-0.200209 1.15464 Reaction Moment(N.m) 0 0 0 0 Reference Geometry-2 Entities: 1 face(s) Reference: Edge< 1 > Type: Use reference geometry Translation: ---, ---, 0 Units: mm Resultant Forces Components X Y Z Resultant Reaction force(n) -1833.89 0-13.1588 1833.94 Reaction Moment(N.m) 0 0 0 0 Entities: Type: 1 face(s) Symmetry Symmetry-1 Resultant Forces Components X Y Z Resultant Reaction force(n) 1833.91 0 0.704849 1833.91 Reaction Moment(N.m) 0 0 0 0 Load name Load Image Load Details Analyzed with SOLIDWORKS Simulation Simulation of RF HEat Test 5

Pressure-1 Entities: 4 face(s) Type: Normal to selected face Value: 150 Units: psi Phase Angle: 0 Units: deg Connector Definitions No Data Contact Information No Data Analyzed with SOLIDWORKS Simulation Simulation of RF HEat Test 6

Mesh information Mesh type Mesher Used: Automatic Transition: Include Mesh Auto Loops: Jacobian points Element Size Tolerance Mesh Quality Solid Mesh Standard mesh On Off 4 Points 0.0301837 in 0.00150918 in High Mesh information - Details Total Nodes 10634 Total Elements 6766 Maximum Aspect Ratio 4.5711 % of elements with Aspect Ratio < 3 99.9 % of elements with Aspect Ratio > 10 0 % of distorted elements(jacobian) 0 Time to complete mesh(hh;mm;ss): 00:00:01 Computer name: DAVID-PC Analyzed with SOLIDWORKS Simulation Simulation of RF HEat Test 7

Sensor Details No Data Resultant Forces Reaction forces Selection set Units Sum X Sum Y Sum Z Resultant Entire Model N 0.0112407 0-0.200209 0.200524 Reaction Moments Selection set Units Sum X Sum Y Sum Z Resultant Entire Model N.m 0 0 0 0 Analyzed with SOLIDWORKS Simulation Simulation of RF HEat Test 8

Beams No Data Analyzed with SOLIDWORKS Simulation Simulation of RF HEat Test 9

Study Results Name Type Min Max Stress1 VON: von Mises Stress at Step No: 285376 N/m^2 2.46521e+008 N/m^2 3667(110.01 Seconds) Node: 10557 Node: 7743 RF HEat Test-Stress One Third Emissivity-Stress-Stress1 Name Type Min Max Displacement1 URES: Resultant Displacement 2.18252e+011 mm 2.18252e+011 mm at Step No: 15000(450 Seconds) Node: 1 Node: 1 Analyzed with SOLIDWORKS Simulation Simulation of RF HEat Test 10

RF HEat Test-Stress One Third Emissivity-Displacement-Displacement1 Name Type Min Max Strain1 ESTRN: Equivalent Strain at Step 5.03211e-007 0.000650753 No: 100(3 Seconds) Element: 2177 Element: 3079 Analyzed with SOLIDWORKS Simulation Simulation of RF HEat Test 11

RF HEat Test-Stress One Third Emissivity-Strain-Strain1 Conclusion Analyzed with SOLIDWORKS Simulation Simulation of RF HEat Test 12