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E106 Lecture Problem 136

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Plane strain toughness definition. Circumferential wall stress ... Plane Strain Toughness Definition. Y = 1.0 for sphere, a = crack length ... – PowerPoint PPT presentation

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Title: E106 Lecture Problem 136


1
E106 Lecture Problem 136
  • David Schimon
  • March 7, 2006

2
Problem Statement
  • Caluate the maximum radius and wall thickness of
    a spherical pressure vessel made of Ti-6Al-4V
    Titanium alloy periodically pressurized to 500
    kPa, s.t. it will leak before breaking.

3
Given Information
  • For Titanium Alloy Ti-6Al-4V,
  • syield 910 MPa
  • KIc 55 MPa sqrt(m)
  • Relevant forumlae
  • Plane strain toughness definition
  • Circumferential wall stress
  • Design Objective leak-before-break

4
Formulae
  • Plane Strain Toughness Definition
  • Y 1.0 for sphere, a crack length
  • Circumferential wall stress
  • p pressure, t thickness, r radius

5
Exploration Leak-before-break
  • In pressure vessels, useful to allow a crack to
    propagate fully through the wall so that gas will
    detectably leak before catastrophically failing.
  • To allow for this, let the thickness of the wall
    be half the critical crack length, or
  • ac t rather than ac t/2
  • This allows gas to leak through before fracture.

6
Revised Formulae
  • Include yield stress and leak criterion
  • Solve for t and combine

7
Plugging and Chugging
8
Conclusions
  • Extremely useful for defining upper bounds
  • Important in determining safety measures
  • A useful method to identify the ability of
    materials to leak before breaking
  • The constant term is a good measure of
    this effectiveness titanium alloy has a value
    of 3.3, while mild steel is 11.2
  • Requires a balance of ductility and yield
    strength

9
The End
  • ?
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