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iga/validation/README.md

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This folder contains the validation cases:
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- [Buckling Analysis](buckling_analysis/README.md)
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- [Cantilever Beam - Multi Patch - Geometric Non-Linear Analysis](cantilever_beam_multi_patch_non_linear/README.md)
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- [Cantilever Beam - Single Patch - Geometric Non-Linear Analysis](cantilever_beam_single_patch_non_linear/README.md)
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- [Plate with Hole - Trimmed Patch - Linear Analysis](plate_with_hole_trimmed_patch_linear/README.md)
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- [Buckling Analysis - Single Patch - Cantilever Beam](buckling_analysis_single_patch_cantilever/README.md)
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- [Geometric Non-Linear Analysis - Multi Patch - Cantilever Beam](geometric_nonlinear_analysis_multi_patch_cantilever_beam/README.md)
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- [Geometric Non-Linear Analysis - Single Patch - Cantilever Beam](geometric_nonlinear_analysis_single_patch_cantilever_beam/README.md)
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- [Plate with Hole - Trimmed Patch - Linear Analysis](geometric_linear_analysis_trimmed_patch_plate_with_hole/README.md)
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- [Scordelis-Lo Roof - Single_Patch - Linear Analysis](scordelis_lo_roof_single_patch_linear/README.md)

iga/validation/buckling_analysis/source/geometry.cad.json

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# Buckling Analysis
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# Buckling Analysis - Single Patch - Cantilever Beam
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**Author:** Aakash Ravichandran
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**Kratos version:** 10.2
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**Source files:** [Buckling Analysis](https://github.com/KratosMultiphysics/Examples/tree/master/iga/validation/buckling_analysis/source)
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**Source files:** [Buckling Analysis - Single Patch - Cantilever Beam](https://github.com/KratosMultiphysics/Examples/tree/master/iga/validation/buckling_analysis/source)
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## Problem definition
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This example presents the validation of buckling analysis in Kratos with Isogeometric Analysis.
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![Reference Model](data/Reference_Model.png)
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<div align="center">
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<img src="data/Reference_Model.png" alt="Displacement" width="600">
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*Structural System [1]*
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</div>
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The cantilever beam is modeled using single NURBS patch with the Shell3pElement. The CAD model of both the patches is constructed with single span B-spline surfaces and has a curve degree of 2 in both axes. Additional refinement is applied in Kratos, by increasing the curve degree to 4 in both axes and inserting 4 knots in the width and 20 knots along the length of the beam.
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The cantilever beam is modeled using single NURBS patch with the Shell3pElement. The CAD model is constructed with single span B-spline surfaces and has a curve degree of 2 in both directions of the plane. Additional refinement is applied in Kratos, by increasing the curve degree to 4 in both axes and inserting 4 knots in the width and 20 knots along the length of the beam.
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## Results
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The buckling load factors are shown in table below. The corresponding buckling modes are shown in image below.
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| Quantity | Reference | Kratos |
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<div align="center">
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| | Reference | Kratos |
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| :--- | :--- | :--- |
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| $\lambda_{cr}^{(1)}$ | 4.1123 | 4.06977 |
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| $\lambda_{cr}^{(2)}$ | 16.449 | 16.1693 |
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| $\lambda_{cr}^{(3)}$ | 37.011 | 36.6759 |
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| $\lambda_{cr}^{(4)}$ | 102.81 | 102.106 |
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</div>
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| Buckling Mode Shape 1 | Buckling Mode Shape 2 |
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| :---: | :---: |
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| ![Buckling Mode Shape 1](data/Buckling_Mode_1.png) | ![Buckling Mode Shape 2](data/Buckling_Mode_2.png) |

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