Numerical simulation of self-sustained oscillations of an airfoil at a transitional reynolds number using high-order schemes

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.2514/6.2011-2139
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Affiliation
  1. National Research Council of Canada. Aerospace
FormatText, Article
Conference52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 4 April 2011 through 7 April 2011, Denver, CO
SubjectCentral differencing schemes; Compressible Navier-Stokes equations; Computer clusters; Differencing scheme; Dual time stepping method; Fully-coupled; Gauss-Seidel relaxation; High-order scheme; Initial solution; Inviscid fluxes; Low-amplitude; Message passing interface; Parallel Computation; Pitching motion; Preconditioning method; Self-sustained oscillations; Small amplitude; Structure dynamics; Subgrid scale models; Temporal terms; Time marching; Weighted essentially nonoscillatory scheme; Airfoils; Computational fluid dynamics; Computer simulation; Experiments; Message passing; Navier Stokes equations; Reynolds number; Structural dynamics; Iterative methods
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LanguageEnglish
Peer reviewedYes
NPARC number21271482
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