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Flow analysis of a flapping SD7003 airfoil at transitional reynolds numbers

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.2514/6.2009-3955
AuthorSearch for: 1; Search for: 1
Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
FormatText, Article
Conference27th AIAA Applied Aerodynamics Conference, June 22-25, 2009, San Antonio, TX; USA
Abstract
This paper presents recent progress of the research performed as part of the NRC's participation in the NATO AVT-149 Unsteady Low-Re Aerodynamics Task Group. Results obtained using the NRC-IAR in-house code INSflow on an SD7003 airfoil compared with experimental results from the US Air Force Research Laboratory (AFRL) indicate that fully three-dimensional (3D) flow separation and stall occur during the flapping motions.
Publication date
PublisherAmerican Institute of Aeronautics and Astronautics
Access condition
  • available
  • unclassified
  • unlimited
In
  • 27th AIAA Applied Aerodynamics Conference.
LanguageEnglish
Peer reviewedYes
NRC numberAL-2008-0074
NPARC number8932574
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Record identifier6b7df0a6-ca43-4460-a55a-505cede2281a
Record created2009-04-23
Record modified2020-04-16
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