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Hoop, Axial and Radial Stresses in Thick-Walled Pressure Vessels
Problem Specification
A simply-supported beam of rectangular cross-section is point loaded at some arbitrary point along its length as shown in figure below.
[!2dbeam_ps.png|width=350!|^2dbeam_ps.png]
_P_ = 10,000 lb, _L_ = 100 in, _a_ = 75 in, _b_ = 3 in, _h_ = 8 in
The material is structural steel with Young's modulus _E_= 2.9e7 psi and Poisson's ratio of 0.3. Using ANSYS Mechanical, find the finite-element solution for non-dimensionalized maximum deflection defined as:
!2dbeam_eq1.png!
Compare the finite-element solution for plane stress and plane strain to Euler-Bernoulli beam theory. Discuss the comparison between the finite-element and beam theory results. Note that the non-dimensionalized maximum deflection is independent of the Young's modulus.
Learning Goals
The purpose of this tutorial is to showcase, in a relatively simple situation, where thin-wall pressure vessel theory is no longer as valid as it is in the limit of large radius-to-thickness ratios. The point is that inadequate theory should not be used for validation purposes in the limit that the physical assumptions on which the theory is based break down. In this problem, this happens gradually as the vessel walls become thicker. This tutorial is meant to highlight where it is relatively straightforward to apply axisymmetric FEA and resolve a solution correctly that disprove analytical treatment with simple formulae derived for thin-walled vessels.
Continue to [Step 1 - Pre-Analysis and Start-Up|SIMULATION:Pressure Vessel - Pre-Analysis & Start-Up]
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