Objective: To find the nodal displacement, stress in each material and reaction force at the support for the plate shown below. Consider the self weight of the plate in addition to the load P = 444.82 N.(Material property: E = 206.842 GPa, ν = 0.3, ρ = 7850 kg/m3)
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Perform free vibration analysis of the system shown in Figure 1. The system contains a cantilever beam whose free end is attached to two springs one in axial direction and other in transverse direction. A mass of 3.5 kg is attached to the middle of the beam.
View PDF PDF -1575 KBObjective: To find the deflection, stress, strain, shear force and bending moment diagram of simply supported beam with uniformly distributed load and point load as shown in Figure
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Objective: Compute the first 20 eigen values of a three layer composite plate shown in Figure 1 of lamina thickness 1/2/1, lamina angle 00/900/00 for the given material property.
View PDF PDF -1213 KBObjective: Extract 10 critical load factors for the cylindrical model shown in the figure.
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Objective: Find the temperature distribution on a rectangular plate
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