JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD
JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD B.Tech III FINITE ELEMENT TECHNIQUES Previous Question Paper (September - 2021 - R15)
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Main
Derive the finite element equation using the potential energy approach and discuss the salient parts.
Answer
The potential energy approach is based on the principle of minimum potential energy, which states that for a stable conservative system, the displacement configuration that satisfies the boundary conditions and equilibrium equations minimizes the total potential energy.
The total potential energy Π is defined as the sum of the internal strain energy (U) and the potential energy of external loads (V):
Substituting the displacement relation {ε} = [B]{u}, where [B] is the strain-displacement matrix:
Defining the stiffness matrix [K] = ∫ [B]^T [D] [B] dV, the expression becomes Π = 0.5 {u}^T [K] {u} - {u}^T {F}. To minimize Π, we take the partial derivative with respect to the nodal displacement vector {u} and set it to zero:
The salient parts include the Stiffness Matrix [K], which represents the structural resistance; the Displacement Vector {u}, representing the unknown nodal degrees of freedom; and the Force Vector {F}, representing the applied external nodal loads.
Explain the various steps involved in solving a problem using finite element method.
Answer
The finite element method follows a systematic procedure to transform a continuous problem into a discrete one:
- Discretization: The domain is divided into a finite number of elements connected at nodes. The geometry and topology are defined by the element type and mesh density.
- Selection of Interpolation Functions: Shape functions are chosen to represent the variation of the field variable (e.g., displacement) within each element, usually expressed as polynomials.
- Element Stiffness Matrix and Load Vector: Using the constitutive laws and strain-displacement relations, the element stiffness matrix [k] and force vector {f} are derived, typically via the principle of minimum potential energy.
- Assembly: Individual element matrices are assembled into a global stiffness matrix [K] and global force vector {F} by enforcing displacement compatibility at shared nodes.
- Application of Boundary Conditions: Known displacements or forces are applied to the global system of equations to remove singularities and ensure a unique solution.
- Solution of Equations: The resulting system of linear algebraic equations [K]{u} = {F} is solved for nodal unknowns using methods like Gaussian elimination or Cholesky decomposition.
- Post-processing: Strains and stresses are calculated from the nodal displacements using the strain-displacement and constitutive matrices.
Consider the bar shown in Figure 1. An axial load P = 200 × 103 N is applied as shown. Using the penalty approach for handling boundary conditions, do the following:
Determine the nodal displacements
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Determine the stress in each material
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Determine the reaction forces.
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For the beam and loading shown in Figure 2, determine the slopes at 2 and 3 and the vertical deflection at the midpoint of the distributed load.
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For the three-bar truss shown in Figure 3, determine the displacements of node 1 and the stress in element 3.
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A two-dimensional plate is shown in Figure 4. Determine the equivalent point loads at nodes 7, 8 and 9 for the linearly distributed pressure load acting on the edge 7-8-9.
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Determine the stiffness matrix for the element shown in Figure 5. Assume plane strain condition. Take E = 210 GPa, ν = 0.3 and t = 10 mm.
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An axisymmetric body with a linearly distributed load on the conical surface is shown in Figure 6. Determine the equivalent point loads at nodes 2, 4 and 6.
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A composite wall consists of three materials as shown in Figure 7. The outer temperature is T0 = 200°C. Convection heat transfer takes place on the inner surface of the wall with T∞ = 800°C and h = 25 W/m2°C. Determine the temperature distribution in the wall.
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