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Asymptotic Analysis of Passive Nonlinear Suppression of Aeroelastic Instabilities of a Rigid Wing in Subsonic Flow.

Oleg V. GendelmanAlexander F. VakakisLawrence A. BergmanD. Michael McFarland
Published in: SIAM J. Appl. Math. (2010)
Keyphrases
  • asymptotic analysis
  • wind tunnel
  • nasa langley research center
  • fluid model
  • flow field
  • state dependent
  • dynamic programming
  • higher level