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An alternating method for analysis of surface-flawed aircraft structural components - MaRDI portal

An alternating method for analysis of surface-flawed aircraft structural components (Q3661061)

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An alternating method for analysis of surface-flawed aircraft structural components
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    An alternating method for analysis of surface-flawed aircraft structural components (English)
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    1983
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    flow chart
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    alternating method
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    quarter-elliptical corner crack
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    completely general analytical solution
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    embedded elliptical crack
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    infinite solid
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    arbitrary crack-face tractions
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    implemented
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    inexpensive procedure for routine evaluation of accurate stress intensity factors
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    flawed structural components
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    brick subject to remote tension
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    emanating from hole in finite-thickness plates subject to remote tension as well as bearing pressure
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    emanating from pin hole
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    aircraft attachment lugs subject to simulated pin loading
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