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Virginia Polytechnic Institute and State University

Plane strain fracture toughness testing of hollow aluminum bars

Abstract

dc:description.abstract

There are certain disadvantages to using round bars for plane strain fracture toughness testing. Specifically these are: (1) a large amount of material is required, for specimen fabrication, (2) a testing machine of great capacity is needed to fail such specimens, (3) there is considerable difficulty and expense involved in precracking the specimens. In attempt to Obtain a specimen free of these disadvantages, a hollow circumferentially notched round configuration has been suggested for plane strain fracture toughness testing. The effect of notch root radius and axial hole diameter were experimentally determined for hollow notched round aluminum bars of half inch outside diameter. From the results of the fracture toughness tests of these half inch specimens, it was concluded that a specimen of larger diameter was necessary in order to produce valid K<sub>IC</sub> results. The equation used to calculate K<sub>IC</sub> for hollow round bars was used to determine optimum dimensions for hollow round specimens. Several 7075-T651 aluminum. specimens of the analytically determined dimensions ' were failed and the corresponding apparent K<sub>IC</sub> calculated. The resulting apparent K<sub>IC</sub> values fell within an acceptable range of the true K<sub>IC</sub>. It may be concluded that optimum dimensions may be analytically determined for hollow round plane strain fracture toughness specimens which will yield a reasonably accurate apparent K<sub>IC</sub>.

Degree

thesis:*
Name thesis:degree_name
Master of Science
Level thesis:degree_level
masters
Discipline thesis:degree_discipline
Engineering Mechanics
Department dc:contributor.department
Engineering Mechanics
Grantor dc:publisher
Virginia Polytechnic Institute and State University
Year dc:date.issued
1970

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Sawyer, Samuel Owen

Rights

dc:rights
Statement dc:rights
  • In Copyright
Language dc:language.iso
en_US

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/10919/71049
OAI identifier oai:identifier
oai:vtechworks.lib.vt.edu:10919/71049

Chain of custody

source
Harvested from
Virginia Tech
Base URL
vtechworks.lib.vt.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
related terms
citation

Sawyer, Samuel Owen. Plane strain fracture toughness testing of hollow aluminum bars. masters thesis, Virginia Polytechnic Institute and State University, 1970. http://hdl.handle.net/10919/71049