Challenge

Challenge 2- Comparing the performance of three types of beams under bending load.

COMPARING THE PERFORMANCE OF THREE BEAM UNDER BENDING LOAD

AIM:- To compare the performance of three beam of different type under bending load.

INTRODUCTION:-This report presents the results of nonlinear analysis performed on three different cross section beam: Rectangular Beam of dim. 80x45 , I section Beam having flange of width 40 mm and web of length 54.83 mm and a C section beam of depth 80mm and flange of width 45 mm and applying a load of 1500 N on the smaller face (i.e. 40 mm for case 1, 45 mm for case 2 and 45 mm face for case 3 ). and fixed on one side and applying load of 1500 N on smaller length face.

Simulation Setup

  • Software Used: SolidWorks Non-Linear Analysis

  • Material: Alloy Steel (Mechanical Properties considered from standard data)

    • Young’s Modulus: ~210 GPa

    • Poisson’s Ratio: ~0.3

    • Yield Strength: ~620.422 MPa (Assumed, may vary based on grade)

    • Ultimate Tensile Strength: ~723.83 MPa

  • Loading Conditions:

    • Load Applied: 1500N

    • Application Side: Smaller side of the beams

    • Support Condition: Fixed at one end

  • Mesh Type: Tetrahedral elements (Fine mesh refinement near high-stress areas)

  • Analysis Type: Non-Linear Static Analysis

1.Beam Geometry & Mass Properties

PROPERTIESI BEAMC-SECTION BEAM80X45 RECT BEAM
Mass ( kg) 2.363593.2226611.088
Volume (m^3)0.000306960.0004185270.00144
Weight (N)23.163231.582108.662

2. Mesh Details

PARAMETERI SECTION BEAM C-SECTION BEAM80X45 RECT BEAM
MESH TYPESOLID MESH SOLID MESHSOLID MESH
MAX ELEMENT SIZE(mm)6.863727.48220511.2949
MIN ELEMENT SIZE (mm) 2.287882.4939911.2949
Total Nodes 57,82428,55611,549
Total Elements 31,98615,3157,282
MESH QUALITYHIGHHIGHHIGH

3 Comparison and Key Observation

3.1Rectangular Beam

  • Maximum Stress: 7.602 MPa (from the simulation image)

  • Maximum Deformation:3.102X10^-2 mm at length of 400mm

  • Stress analysis: The rectangular beam has an intermediate stress level but lacks the weight efficiency of the beam.

  • Deformation Analysis: it has moderate displacement value 0.03102 suggesting it stable but more heavier than the I beam.


3.2 I Section Beam

  • Maximum Stress: 2.58X10^7Pa

  • Maximum Deformation: 8.569X10^-02mm

  • Stress analysis: The I beam experience the maximum highest on Mises stress (2.583e+07 N/m²), but remains well within its yield strength, indicating high structural efficiency.

  • Deformation Analysis: Deformation is maximum among three i.e. it deforms the most under load i,e 0.08569 mm


3.3 C-Section Beam

  • Maximum Stress: 2.55x10^4 Pa at the fixed end

  • Maximum Deformation: 2.022x10^-4 mm

  • Stress analysis: The C section Beam observed lowest stress level but may be prone to buckling or torsional instability due to its open profile

  • Deformation Analysis: Deformation is lowest among three indicating better stiffness but potential instability.

4.Conclusions:-

  1. Best Beam for Efficiency & Strength: The I-Beam takes the top spot since it resists heavy loads efficiently while making the best use of material.
  2. Best Beam with Least Deflection: The C-Section Beam has minimal displacement but may require additional support to prevent buckling.
  3. Best Beam for Simplicity and Stability: The 80x45 Rectangular Beam strikes a good balance between simplicity and stability, though it is on the heavier side.

5. Recommendation:-

If you require the optimal balance of strength and weight efficiency, the I-Beam is the preferred choice. When buckling is a concern, the C-Section Beam performs well with additional support. For applications where weight is not a critical factor, the Rectangular Beam remains a reliable option.

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