A Higher-Order Theory for Fiber-Metal Laminates under Generalized Plane Stress Conditions

From National Research Council Canada

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Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
  2. Carleton University
FormatText, Article
SubjectFiber-metal laminates; fatigue crask; stress intensity factor
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NRC numberSMPL-2005-0184
NPARC number8931569
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Record identifier43b7e7fa-8fbe-46ca-8475-cacd8ebca0e3
Record created2009-04-23
Record modified2020-04-16
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