Steady State Crack Growth Prediction Method for Glare and Advanced FMLs

Gregory Wilson, René Alderliesten
  • May 2009, American Institute of Aeronautics and Astronautics (AIAA)
  • DOI: 10.2514/6.2009-2589

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http://dx.doi.org/10.2514/6.2009-2589

The following have contributed to this page: Dr René C Alderliesten