JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD
JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD B.Tech III FINITE ELEMENT METHODS Previous Question Paper (August/September - 2021 - R18)
Answer any five questions. All questions carry equal marks.
Main
Discuss advantages, limitations and applications of FEM.
Answer
The Finite Element Method (FEM) is a numerical technique for finding approximate solutions to boundary value problems. Its advantages include the ability to handle complex geometries, irregular boundaries, and non-homogeneous materials. It effectively models different loading conditions and boundary constraints, making it highly versatile for structural, thermal, and fluid analysis.
Limitations include high computational requirements for complex 3D models, sensitivity to mesh quality, and the potential for significant errors if input parameters or boundary conditions are incorrectly defined. It also requires specialized software and expertise to interpret results accurately.
Applications are widespread across engineering disciplines, including stress analysis of machine components, heat transfer analysis, fluid flow simulation, vibration and modal analysis, and crashworthiness testing in automotive and aerospace industries.
Explain plane stress and plane strain conditions with suitable examples.
Answer
Plane Stress occurs in thin plates where the thickness is significantly smaller than the other dimensions, and the loads act only in the plane of the plate. In this condition, the stress components perpendicular to the plate surface are assumed to be zero (σz = τxz = τyz = 0). An example is a thin sheet metal component subjected to in-plane tensile or compressive forces.
Plane Strain occurs in long, prismatic structures where the cross-section remains constant along the length, and the loading is uniform along that length. In this condition, the strain components perpendicular to the cross-section are assumed to be zero (εz = γxz = γyz = 0). An example is a long dam or a thick-walled pipe under internal pressure, where the longitudinal deformation is constrained by the geometry.
Derive the stiffness matrix and consistent load vector for one dimensional quadratic element.
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Find the nodal displacements and stresses in horizontal member and support reactions of truss shown in the below figure 1.
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Determine the displacement at the midpoint of a fixed beam of length 1 m with uniformly distributed load of 6 kN/m through the span. Use two beam elements. Take E = 200 GPa and El = 2 × 104 N.m2.
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Determine the stiffness matrix for the constant strain triangular (CST) element shown in the figure 2. The coordinates are given in units of millimetres. Assume plane stress conditions. Take E = 200 GPa; Poisson’s ratio (v) = 0.3; Thickness (t) = 10 mm.
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Derive Shape functions four- node quadrilateral Element and discuss salient points.
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Evaluate the integral by applying one and two-point point Gaussian quadrature. Compare the results with exact results and comment.
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For the composite wall shown in the figure 3 below, compute the interface temperatures considering three elements. Take K1=5 W/m-K, K2=0.6 W/m-K, K3=20 W/m-K, T1=1000C, T4=4000C.
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Derive consistent mass matrix for truss element and also write the lumped mass matrix for the same element.
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Discuss the importance of semi-automatic meshing and auto mesh along with the practical applications.
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