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  • Structural Mechanics  (1)
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    Flaw Growth of 6Al-4V Titanium in a Freon TF Environment (1969)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: The plane strain threshold stress intensity and sustained stress flaw growth rates were experimentally determined for 6AI-4V S.T.A. titanium forging and weldments in environments of Freon TF at room temperature. Sustained load tests of surface flawed specimens were conducted with the experimental approach based on linear elastic fracture mechanics. It was concluded that sustained stress flaw growth rates, in conjunction with threshold stress intensities, can be used in assessing the service life of pressure vessels.
    Keywords: Structural Mechanics
    Type: NASA-CR-99632
    Format: application/pdf
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