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      by 
      Barr, Stephen M., author. (orcid)0000-0002-0450-165X
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      loads and structural deformations of the blades, respectively, which are passed iteratively between the
      by 
      Ward, Elizabeth, author. (orcid)0000-0001-6057-2711
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      analysis was performed using a full 3-D FEA based aeroelastic computational structural dynamics (CSD
      by 
      Zeng, Chen, author.
      Format: 
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      -controls and structural analysis was performed (by other researchers) in a parallel effort to complement this
      by 
      Strilchuk, Pedro Martin Mendoza, author.
      Format: 
      Alıntı: 
      potentially affect the dynamics and control of the vehicle. In addition, in-flight structural loads will