FEMAP HEEL TOE PROBLEM / SOL 101/SOL401/SOL106
Support Files: https://emafd.com/wp-content/uploads/2021/11/video_files.zip
FEMAP SEMI MONOCOQUE / STIFFENED PANEL STRUCTURE
Support Files: https://emafd.com/wp-content/uploads/2021/10/video.zip
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FEMAP: STATIC & MODAL SOLUTIONS FOR SIMPLY SUPPORTED FILE
Support Files: https://emafd.com/wp-content/uploads/2021/10/validation_plate_uniform.zip
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FEMAP: MULTI STEPS MECHANICAL SOL 101 AND SOL 109
Support Files: https://emafd.com/wp-content/uploads/2021/09/femap_multi_steps_mechanical.zip
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FEMAP: BUCKLING LOAD OF CANTILEVER BEAM USING SOL 105 AND SOL 106
Supporting Files: https://emafd.com/wp-content/uploads/2021/08/femap_buckling_sol_105_106.zip
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FEMAP: SIMPLY SUPPERTED BEAM, LARGE DEFORMATION, NONLINEAR STATIC SOLUTION 106
Supporting Files: https://emafd.com/wp-content/uploads/2021/08/femap_simply_supported_beam_nonlinear.zip
FEMAP: CANTILEVER BEAM, LARGE DEFORMATION, NONLINEAR STATIC SOLUTION 106
Supporting Files: https://emafd.com/wp-content/uploads/2021/08/femap_beam_large_deflection.zip
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FEMAP: BASE EXCITATION (SOL 109)
Supporting files: https://emafd.com/wp-content/uploads/2021/07/base_excitation_femap.zip
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FEMAP: 2DOF MASS-SPRING SYSTEM
Supporting Files: https://emafd.com/wp-content/uploads/2021/04/2dof_vibrations.zip
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FEMAP: STRESS AROUND CIRCULAR HOLE USING SOLID ELEMENTS
You can download the FEMAP file from previous video (Stress around hole using shell elements) and follow the steps.
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FEMAP: STRESS AROUND CIRCULAR HOLE USING SHELL ELEMENTS
SUPPORT FILES: https://emafd.com/wp-content/uploads/2021/03/plate_hole_shell_elements.zip
When post-processing, the normal stresses in 2D elements are normally reported relative to the elemental coordinate systems (which may be different in each element). In order to show the stresses in a direction aligned with the global coordinate system, a transformation from elemental to global coordinate system is needed. This can be accomplished through: View menu > Select > Deformed and Contour Data… > Contour Transformation > Shell Element Output. This solved the customer’s issue.
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FEMAP: MESHING AROUND HOLE USING SOLID ELEMENTS
Meshing around a hole using solid elements. Surface 2-D elements (plate) are created with adequate mesh and then extrude through the thickness of the plate generating 3-D elements (Solid).
https://emafd.com/wp-content/uploads/2021/01/hole_mesh_solid.zip
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FEMAP: Shear Effect Contribution in Cantilever Beam (K Factor)
Validation of FEMAP model of a cantilever beam with end load. Deformation is calculated considering bending and shear effects and FEMAP beam, plate, and solid models are developed.
Quick Note: Remember that in general plate/shell elements are not good in shear and solid elements are not good in bending for thin structures
Support Files: https://emafd.com/wp-content/uploads/2020/12/beam_shear_factor.zip
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FEMAP: RB2 to Connect Beam to Plate/Solid Elements
Validation and video of connecting beam elements to either plate or solid elements. RB2 add stiffness to the model so attention must be given to the amount of RB2 used when creating a connection.
Support Files: https://emafd.com/wp-content/uploads/2020/12/support_files_rb2_connections.zip
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FEMAP: Connection Between Solid and Plate Elements (Glue Connection)
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FEMAP TAPERED SHEAR PANEL SOL101
FEMAP WING BOX ANALYSIS
FEMAP 2-D WING SPAR PART 1
FEMAP 2-D WING SPAR PART 2
FEMAP 3-D WING SPAR
FEMAP: TRUSS DEFORMATION OF STAICALLY DETERMINATED PROBLEM USING CASTIGLIANOS’