A Stress Analysis Method for Bi-axially loaded fastener hole in a laminate of finite geometry

From National Research Council Canada

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  1. National Research Council of Canada. NRC Institute for Aerospace Research
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NRC numberSMPL-1997-0079
NPARC number8933296
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Record identifiera26cc8f7-b6b1-43e5-ab5c-7e83d48b1fc2
Record created2009-04-23
Record modified2020-03-03
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