The finite element method (FEM) is the most widely used method for solving problems of engineering and mathematical models. Typical problem areas of interest include the traditional fields of structural analysis, heat transfer, fluid flow, mass transport, and electromagnetic potential. The FEM is a particular numerical method for solving partial differential equations in two or three space variables .To solve a problem, the FEM subdivides a large system into smaller, simpler parts that are called finite elements. This is achieved by a particular space discretisation in the space dimensions, which is implemented by the construction of a mesh of the object: the numerical domain for the solution, which has a finite number of points. The finite element method formulation of a boundary value problem finally results in a system of algebraic equations. The method approximates the unknown function over the domain. The simple equations that model these finite elements are then assembled into a larger system of equations that models the entire problem. The FEM then uses variational methods from the calculus of variations to approximate a solution by minimizing an associated error function.

FEM is best understood from its practical application, known as finite element analysis (FEA). FEA as applied in engineering is a computational tool for performing engineering analysis. It includes the use of mesh generation techniques for dividing a complex problem into small elements, as well as the use of software program coded with FEM algorithm. In applying FEA, the complex problem is usually a physical system with the underlying physics such as the Euler-Bernoulli beam equation, the heat equation, or the Navier-Stokes equations expressed in either PDE or integral equations, while the divided small elements of the complex problem represent different areas in the physical system.

Visualization of how a car deforms in an asymmetrical crash using finite element analysis
BEAM :-

A beam is a structural element that primarily resists loads applied laterally to the beam's axis. Its mode of deflection is primarily by bending. The loads applied to the beam result in reaction forces at the beam's support points. The total effect of all the forces acting on the beam is to produce shear forces and bending moments within the beam, that in turn induce internal stresses, strains and deflections of the beam. Beams are characterized by their manner of support, profile (shape of cross-section), equilibrium conditions, length, and their material.

Classification based on supports :-

In engineering, beams are of several types:-

  • Simply supported – a beam supported on the ends which are free to rotate and have no moment resistance.
  • Fixed – a beam supported on both ends and restrained from rotation.
  • Over hanging – a simple beam extending beyond its support on one end.
  • Double overhanging – a simple beam with both ends extending beyond its supports on both ends.
  • Continuous – a beam extending over more than two supports.
  • Cantilever – a projecting beam fixed only at one end.
  • Trussed – a beam strengthened by adding a cable or rod to form a truss.

PROCEDURE :-

  • Firstly, Create 2D sketch of the beams as per the given problem statement.
  • Then extrude the 2D sketch to about 400mm to create 3D model of the beams.

Models-

CASE-1

Fig:-Cross section of beam 1

Fig:-3D Model of beam 1

CASE-2

Fig:-Cross section of beam 2

Fig:-3D Model of beam 2

CASE-3

Fig:-Cross section of beam 3

Fig:-3D Model of beam 3

  • Solidwork Simulation -> Select Static Study
  • Apply Materials to the beam -> Alloy Steel

Apply Constraints -> Fixture -> Fixed symmetry

CASE-1

CASE-2

CASE-3

Apply Bending Load -> Force -> Select the 45mm, 40mm, 45mm face of beam 1, 2 and 3 respectivly = 1500N

CASE-1

CASE-2

CASE-3

Apply Mesh -> Unit = mm -> Size = 5mm and Tolerance = 0.25mm

CASE-1

CASE-2

CASE-3

RESULTS :-

CASE-1 (Rectangular beam)

Stress Plot :-

Strain Plot :-

Displacement Plot :-

CASE-2 (I-Shaped beam)

Stress Plot :-

Strain Plot :-

Displacement Plot :-

CASE-3 (C-Shaped beam)

Stress Plot :-

Strain Plot :-

Displacement Plot :-

COMPARISON OF BEAMS :-

Beam Maximum Von Misses Stress(MPa) Maximum Displacement(mm) Maximum Equivalent Strain (MPa)
1 9.624 0.031 3.164e-05
2 23.832 0.086 8.104e-05
3 43.416 0.303 1.214e-05

CONCLUSION :-

  • As we can see the above table summary which depicts that the Stress and Displacement value of the Beam 1 is less than beam 2 so it is best choice beam for our use but it is not economical and its do not fulfill the weight creteria.
  • Beam 3 is the best choice if we consider economical and weight criteria as its strain is very less as compared to other beams and its Stress and Displacement is too high which is also not suitable.
  • Beam 2 is the best choice as it is very good in term of Stress and Displacement and also goog Equivalent Strain due to which less material is used which thereby reduces its weight and cost.
  • So I-Shaped beam(Beam 2) is the Best Choice among all beams.