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A Century of Active Control of Boundary Layer Separation: A Personal View

  • Israel J. Wygnanski
Part of the Solid mechanics and its applications book series (SMIA, volume 129)

Keywords

Boundary Layer Pressure Recovery Boundary Layer Separation Periodic Excitation Circulation Control 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Reference

  1. [1]
    A. Betz, Boundary Layer Control in Germany, Boundary layer and flow control, its principles and application, G.V. Lachmann ( ED), Pergamon Press NY., 1961.Google Scholar
  2. [2]
    S. Goldstein, Fluid Mechanics in the first half of this century, Annual Reviews of Fluid Mechanics 1, 1-28, 1969.CrossRefGoogle Scholar
  3. [3]
    A. Baumann, Tragflugel fur Flugzeugemit Luftraustrittsoffnungen in der Ausenhaut, Deutsches Reichs Patent 400806, 1921.Google Scholar
  4. [4]
    Schrenk, O., Versuche an einem Absaugflugel, ZFM 22, p. 259, 1931.Google Scholar
  5. [5]
    J. Legras, Contribution Theorique a L’effet de puit C.R. Acad. Sc. Paris, 1947.Google Scholar
  6. [6]
    Schwier W., Auftriebsanderung Durch Einem auf der Flugeldruckseite Ausgeblasenen Luftstrahl UM31912, 1944.Google Scholar
  7. [7]
    Ph. Poisson-Quinton & L. Lepage French Research on Control of Boundary Layer and Circulation in: Boundary layer and flow control, its principles and application. (Lachmann, G.V.-editor), Pergamon Press, New York, 1961.Google Scholar
  8. [8]
    Spence, D.A. The Lift Coefficient of a Jet-Flapped Wing. Proc. Roy. Soc. A Vol. 238, p. 46, 1956.MATHCrossRefMathSciNetGoogle Scholar
  9. [9]
    Legendre, R. Influence de l’Emission d’un Jet au bord de Fuite d’un Profil sur l’Ecoulement autour de ce Profil. Comptes Rendus, Académie des Sciences, Paris, 1956.Google Scholar
  10. [10]
    Woods, L.C. Some Contributions to Jet-Flap Theory and to the Theory of Source Flow from Aerofoils. A.R.C. Current Paper 388, 1958.Google Scholar
  11. [11]
    Malavard, L. Sur une Théorie Lineaire du Soufflage au bord de Fuite d’un Profil d’Aile. Comptes Rendus, Académie des Sciences, Paris, 1956.Google Scholar
  12. [12]
    Davidson, I.M., The jet flap J. Royal Aero. Soc. Vol. 60, pp. 25, 1956.Google Scholar
  13. [13]
    Wygnanski, I. & Newman, B. G. The effect of jet entrainment on lift and moment for a thin airfoil with blowing. Aeronautical Quarterly, Vol. XV, p. 122, 1964.Google Scholar
  14. [14]
    Wygnanski, I., “The Effect of Jet Entrainment on Loss of Thrust on a Two- Dimensional Jet-Flap Aerofoil,” Aeronautical Quarterly 17, pp. 31-51, 1966.Google Scholar
  15. [15]
    Nishri B. & Wygnanski I. (1998) Effects of periodic excitation on turbulent flow separation from a flap. AIAA Journal 38 (4).Google Scholar
  16. [16]
    Darabi A. On the mechanism of forced flow reattachment. PhD Thesis, Tel Aviv University, 2000 Also J. Fluid Mechanics 510, 105, 2004.MATHCrossRefGoogle Scholar
  17. [17]
    D. Greenblatt & I. Wygnanski, The control of flow separation by periodic excitation, Progress in Aerospace Sciences 36, 487, 2000.CrossRefGoogle Scholar
  18. [18]
    Williams, J., British Research on Boundary Layer Control for High Lift. Boundary layer and flow control, its principles and application. (Lachmann, G.V.-editor), Pergamon Press, New York, 1961.Google Scholar
  19. [19]
    I. Wygnanski,The Variables Affecting the Control of Separation by Periodic Excitation. AIAA paper 2004-2505, 2004.Google Scholar
  20. [20]
    H. Nagib & J. Kiedaisch, A new look at scaling parameters for evaluating effectiveness of active control of separation, AIAA 2003-0056, 2003.Google Scholar

Copyright information

© Springer 2006

Authors and Affiliations

  • Israel J. Wygnanski
    • 1
  1. 1.AME DepartmentThe University of ArizonaTucsonUSA

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