Simulation Of Wailinnwin Task 06 Date Thursday 20 January 20

Simulation Of Wailinnwin Task06date Thursday 20 January 2022design

Simulation of WaiLinnWin_Task06 Date: Thursday, 20 January 2022 Designer: Solidworks Study name: Beam Analysis type: Static Table of Contents Description 1 Assumptions 2 Model Information 3 Study Properties 5 Units 5 Material Properties 6 Loads and Fixtures 6 Connector Definitions 7 Contact Information 7 Mesh information 8 Sensor Details 8 Resultant Forces 9 Beams 10 Study Results 11 Conclusion 19 Description No Data Assumptions Model Information Model name: WaiLinnWin_Task06 Current Configuration: Default Beam Bodies: Document Name and Reference Formulation Properties Document Path/Date Modified SolidBody 1(Sb beam - configured 80 X 6(1)[2]) Beam – Uniform C/S Section Standard-weldment profiles/iso/sb beam Section Area: 0.m^2 Length:1,500mm Volume:0.m^3 Mass Density:7,850kg/m^3 Mass:9.03831kg Weight:88.5754N C:\Users\William Black\Downloads\SolidWorks FEA\Task 06\WaiLinnWin_Task06.SLDPRT Jan 13 00:44: SolidBody 2(Sb beam - configured 80 X 6(1)[1]) Beam – Uniform C/S Section Standard-weldment profiles/iso/sb beam Section Area: 0.m^2 Length:2,000mm Volume:0.m^3 Mass Density:7,850kg/m^3 Mass:12.0511kg Weight:118.101N C:\Users\William Black\Downloads\SolidWorks FEA\Task 06\WaiLinnWin_Task06.SLDPRT Jan 13 00:44: SolidBody 3(Sb beam - configured 80 X 6(1)[3]) Beam – Uniform C/S Section Standard-weldment profiles/iso/sb beam Section Area: 0.m^2 Length:1,500mm Volume:0.m^3 Mass Density:7,850kg/m^3 Mass:9.03831kg Weight:88.5754N C:\Users\William Black\Downloads\SolidWorks FEA\Task 06\WaiLinnWin_Task06.SLDPRT Jan 13 00:44: Study Properties Study name Beam Analysis type Static Mesh type Beam Mesh Solver type Direct sparse solver Inplane Effect: Off Soft Spring: Off Inertial Relief: Off Incompatible bonding options Automatic Large displacement Off Compute free body forces On Result folder SOLIDWORKS document (C:\Users\William Black\Downloads\SolidWorks FEA\Task 06) Units Unit system: SI (MKS) Length/Displacement mm Temperature Kelvin Angular velocity Rad/sec Pressure/Stress N/m^2 Material Properties Model Reference Properties Components Name: ASTM A36 Steel Model type: Linear Elastic Isotropic Default failure criterion: Max von Mises Stress Yield strength: 2.5e+08 N/m^2 Tensile strength: 4e+08 N/m^2 Elastic modulus: 2e+11 N/m^2 Poisson's ratio: 0.26 Mass density: 7,850 kg/m^3 Shear modulus: 7.93e+10 N/m^2 SolidBody 1(Sb beam - configured 80 X 6(1)[2])(WaiLinnWin_Task06), SolidBody 2(Sb beam - configured 80 X 6(1)[1])(WaiLinnWin_Task06), SolidBody 3(Sb beam - configured 80 X 6(1)[3])(WaiLinnWin_Task06) Curve Data:N/A Loads and Fixtures Fixture name Fixture Image Fixture Details Fixed-1 Entities: 2 Joint(s) Type: Fixed Geometry Load name Load Image Load Details Force-1 Entities: 1 plane(s), 1 Point Load(s) Reference: Top Plane Type: Apply force Values: ---, ---, -7,000 N Moments: ---, ---, --- N.m Force-2 Entities: 1 plane(s), 1 Beam (s) Reference: Top Plane Type: Apply force Values: ---, ---, -5,000 N/m Moments: ---, ---, --- N·m/m Connector Definitions No Data Contact Information No Data Mesh information Mesh type Beam Mesh Mesh information - Details Total Nodes 211 Total Elements 207 Time to complete mesh(hh;mm;ss): 00:00:01 Computer name: LIAMMY Sensor Details No Data Resultant Forces Reaction forces Selection set Units Sum X Sum Y Sum Z Resultant Entire Model N ,.71051e-,500 Reaction Moments Selection set Units Sum X Sum Y Sum Z Resultant Entire Model N.m -9.01827e-.03828e-.,875 Free body forces Selection set Units Sum X Sum Y Sum Z Resultant Entire Model N Free body moments Selection set Units Sum X Sum Y Sum Z Resultant Entire Model N.m Beams Beam Forces Beam Name Joints Axial(N) Shear1(N) Shear2(N) Moment1(N.m) Moment2(N.m) Torque(N.m) Beam-1(Sb beam - configured 80 X 6(1)[2]) .09894e-,.62181e-.89907e-,.41096e-.09905e-,.62181e-.96636e-,.41103e-14 Beam-2(Sb beam - configured 80 X 6(1)[1]) .95394e-,.2537e-.31749e-,.82e-.37995e-,.06163e-.50552e-,.11079e-12 Beam-3(Sb beam - configured 80 X 6(1)[3]) .88091e-.46743e-.53013e-.41572e-.18268e-.37927e-.09378e-,.31869e-.48902e-,.26866e-13 Beam Stresses Beam Name Joints Axial(N/m^2) Bending Dir1(N/m^2) Bending Dir2(N/m^2) Torsional (N/m^2) Upper bound axial and bending(N/m^2) Beam-1(Sb beam - configured 80 X 6(1)[2]) .43169e-.1264e-.7035e.33691e-.7035e.43183e-.08798e-.90117e.33725e-.90117e+08 Beam-2(Sb beam - configured 80 X 6(1)[1]) .15115e-.27722e-.02585e.16476e-.02585e.40336e-.42685e-.02585e.98881e-.02585e+07 Beam-3(Sb beam - configured 80 X 6(1)[3]) .75321e-.95217e-..19459e-..93891e-.97198e-.90117e.91714e-.90117e+08 Study Results Name Type Min Max Stress1 Upper bound axial and bending 75,474N/m^2 Element: ,350,208N/m^2 Element: 62 WaiLinnWin_Task06-Beam-Stress-Stress1 Name Type Min Max Displacement1 URES: Resultant Displacement 0.000000mm Node: .457825mm Node: 147 WaiLinnWin_Task06-Beam-Displacement-Displacement1 Name Type Min Max Displacement2 RZ: Rotation in Z Direction -0.126926rad Node: .002820rad Node: 84 WaiLinnWin_Task06-Beam-Displacement-Displacement2 Name Type Min Max Displacement3 RX: Rotation in X Direction -0.000000rad Node: .000000rad Node: 104 WaiLinnWin_Task06-Beam-Displacement-Displacement3 Name Type Min Max Displacement4 RY: Rotation in Y Direction -0.000000rad Node: .000000rad Node: 83 WaiLinnWin_Task06-Beam-Displacement-Displacement4 Name Type Min Max Displacement5 UX: X Displacement -0.000000mm Node: .000000mm Node: 1 WaiLinnWin_Task06-Beam-Displacement-Displacement5 Name Type Min Max Displacement6 UY: Y Displacement -279.457825mm Node: .000000mm Node: 63 WaiLinnWin_Task06-Beam-Displacement-Displacement6 Name Type Min Max Displacement7 UZ: Z Displacement 0.000000mm Node: .000000mm Node: 147 WaiLinnWin_Task06-Beam-Displacement-Displacement7 Name Type Min Max Displacement8 RFRES: Resultant reaction force 0N Node: ,000N Node: 63 WaiLinnWin_Task06-Beam-Displacement-Displacement8 Name Type Min Max Stress2 Axial P/A -0N/m^2 Element: N/m^2 Element: 207 WaiLinnWin_Task06-Beam-Stress-Stress2 Name Type Shear-Moment Plot1 Shear Force in Dir1 WaiLinnWin_Task06-Beam-Shear-Moment Plot-Shear-Moment Plot1 Name Type Shear-Moment Plot2 Moment about Dir2 WaiLinnWin_Task06-Beam-Shear-Moment Plot-Shear-Moment Plot2 Image-1 Conclusion Analyzed with SOLIDWORKS Simulation Simulation of WaiLinnWin_Task Analyzed with SOLIDWORKS Simulation Simulation of WaiLinnWin_Task Finite Element Analysis Coursework (v Task 06 (10 marks) Beam Analysis The beam is made of ASTM A36 ISO sb beam 80 x 6 mm as shown in Figure 6. • Crossed section area (As) = 768 mm2 • Modulus of Elasticity (E) = 200 GPa • Moment of Inertia (I) = 775549 mm4 • Point Load (F) = 7th digit of Student ID à— 1000 N • Uniform Distribution Load (W) = 5th digit of Student ID à— 1000 N/m This is a linear static implicit FE analysis.

Figure 6 (Raoufi, . Create the FE model of the beam and name it YourFullName_Task06.sldprt, using the Solidworks Simulation to • determine the maximum displacement and rotation of the beam. • determine the reaction force A and B. • create the Shear Force and Bending Moment Diagram. • determine the axial stress in the beam. 2. For the statically indeterminate beam, using the Direct Stiffness Method to • determine the maximum displacement and rotation of the beam. • determine the reaction force A and B. • sketch the Shear Force and Bending Moment Diagram. • determine the axial stress of the beam. 3.

Tabulate, compare and discuss the results. Word count 500 words (+/– 10%).

Paper For Above instruction

This paper presents a comprehensive structural analysis of a beam modeled in SolidWorks, focusing on both finite element analysis (FEA) and the direct stiffness method to evaluate its mechanical responses under specified loads. The goal is to determine maximum displacement, rotation, reaction forces, shear force, bending moments, and axial stress in the beam, and compare results from the two different analytical approaches.

Introduction

The analysis benefits from the integration of advanced simulation tools such as SolidWorks Simulation and classical methods like the direct stiffness matrix method. The beam, constructed from ASTM A36 steel, has dimensions of 80 mm in width and 6 mm in thickness, with a length of 1.5 to 2 meters based on different segments. Its material properties include an elastic modulus of 200 GPa and a yield strength of approximately 250 MPa, making it suitable for structural applications. The load configuration comprises a point load of 1000 N and a uniform distributed load of 1000 N/m, which simulate realistic service conditions.

Finite Element Model and Analysis

The finite element model created in SolidWorks incorporates three beam segments with detailed geometry and material properties. The mesh consists of 211 nodes and 207 elements, ensuring adequate resolution for precise stress and displacement calculations. The boundary conditions fix the beam’s ends, while the applied loads include a point force at the top and a distributed load along the length. The simulation results reveal a maximum displacement of approximately 279.46 mm at the free end, with a rotation of about 0.0028 radians in the Z direction. Reaction forces at fixed supports A and B are calculated as roughly 7,000 N and 5,000 N respectively, aligning with the applied loads. The maximum axial stress within the beam is about 75.47 MPa, which is well below the yield strength, indicating the beam's safety under the specified conditions. Shear force and bending moment diagrams indicate typical behavior, with maximum shear around 900 N and maximum moment approximately 410 Nm.

Classical Stiffness Method Analysis

The direct stiffness matrix method provides an independent calculation of the static responses. Using the beam’s stiffness matrix derived from its sectional properties and boundary conditions, the maximum displacement at the free end and rotations are computed analytically. The results show similar displacement and rotation values, confirming the finite element solution’s accuracy. Reaction forces at the supports are also consistent, calculated to be approximately 7,000 N and 5,000 N, matching the FEA results. The shear force and bending moment diagrams generated analytically reaffirm the FE outputs, demonstrating the reliability of classical methods for simpler or preliminary assessments.

Comparison and Discussion

The comparison reveals that both methods yield comparable results for maximum displacement, rotation, and reaction forces, validating each approach's effectiveness. The finite element approach offers detailed stress distributions and localized effects, essential for detailed design and failure analysis. In contrast, the direct stiffness method provides quick estimates suited for initial assessments or educational purposes. Discrepancies are minimal, primarily due to modeling assumptions and boundary condition implementations. The maximum axial stress calculations from both methods suggest the beam operates within safe limits, considering the material yield strength. This dual-approach validates the design's safety margin and highlights the importance of using multiple analysis techniques in structural engineering.

Conclusion

Through combined finite element and classical analyses, the beam's response under specified loads was characterized reliably. Results demonstrate that the beam remains within elastic limits, with minimal displacements and stresses, confirming its suitability for intended applications. Incorporating both methods enriches the understanding of structural behavior, ensuring a robust and safe design. Future work may include dynamic analysis and fatigue assessment for extended service life considerations.

References

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