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Numerical Study of the Aerodynamic Characteristics of a Multi-Element Airfoil NACA 23012

Journal Article
2013-01-1410
ISSN: 1946-3855, e-ISSN: 1946-3901
DOI: https://doi.org/10.4271/2013-01-1410
Published April 08, 2013 by SAE International in United States
Numerical Study of the Aerodynamic Characteristics of a Multi-Element Airfoil NACA 23012
Sector:
Citation: Gabbasa, A., Jawad, B., Liu, L., and Arslan, S., "Numerical Study of the Aerodynamic Characteristics of a Multi-Element Airfoil NACA 23012," SAE Int. J. Aerosp. 6(1):8-16, 2013, https://doi.org/10.4271/2013-01-1410.
Language: English

References

  1. Zingg , D.W. , Rango , S.D. & Pueyo , A. 2002 Advances in algorithms for computing aerodynamic flows Caughey D.A. & Hafez M.M. Frontiers of computational fluid dynamics 347 380 The United States of America World Scientific Publishers
  2. Kaku , M. 1999 Visions: how science will revolutionize the twenty-first century London Oxford University Press
  3. Abbott Ira H. , von Doenhoff A. E. 1959 Theory of Wing Sections: Including a Summary of Airfoil Data Dover Publications
  4. Versteeg , H. , Malalasekera , W. An introduction to computational fluid dynamics, The Finite Volume Method Second 63 64 2007
  5. Platt , R. and Abbott , I. Aerodynamic characteristics of NACA. 23012 and 23021 airfoils with 20-percentchord external- airfoil flaps of NACA 23012 section National Advisor Committee for Aeronautics 1937
  6. White , F. Viscous Fluid Flow Third 2006
  7. Drag Coefficient & Lifting Line Theory 1997 2012 http://www.aerospaceweb.org/question/aerodynamics
  8. Laminar, Turbulence, Transition and Flow separation 1997 1999 Cislunar Aerospace, Inc. http://wings.avkids.com/Tennis/Book/laminar

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