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Bifurcation Analysis of an Airfoil in Subsonic Flow with Coupled Cubic Restoring Forces

From National Research Council Canada

AuthorSearch for: 1; Search for: 2
Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
  2. University of Texas Pan American
FormatText, Article
ConferenceJournal of Aircraft
Subjectbifurcation; nonlinear aeroelasticity; airfoil; subsonic flow
Access condition
  • available
  • unclassified
  • unlimited
NRC numberAL-2006-0139
NPARC number8928707
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Record identifierb883a1e8-2754-48a3-890e-b3381283a10d
Record created2009-04-23
Record modified2020-04-16
Date modified: