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Virtual zone Navier-Stokes computations for oscillating control surfaces

  • G. H. Klopfer
  • S. Obayashi
3. Numerical Methods and Algorithms d) Euler/Navier-Stokes Equations
Part of the Lecture Notes in Physics book series (LNP, volume 453)

Keywords

AIAA Paper Transonic Flow Rigid Wing Aspect Ratio Wing Flow Field Computation 
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.

References

  1. 1.
    Ballhaus, W., Goorjian, P.M., and Yoshihara, H.; “Unsteady Force and Moment Alleviation in Transonic Flow,” AGARD Conference Proceeding No. 227, May 1981.Google Scholar
  2. 2.
    Guruswamy, G.P. and Tu, E.L.; “Transonic Aeroelasticity of Fighter Wings with Active Control Surface,” Journal of Aircraft, Vol. 26, No. 7, July 1980, pp. 682–684.Google Scholar
  3. 3.
    Steger, J.L. and Bailey, H.E.; “Calculation of Transonic Aileron Buzz,” AIAA Journal, Vol. 18, March 1980, pp. 249–255.Google Scholar
  4. 4.
    Horiuti, K., Chyu, W.J., and Buell, D.A.; “Unsteady Transonic Flow Computation for an Airfoil with an Oscillating Flap,” AIAA Paper 84-1562, June 1984.Google Scholar
  5. 5.
    Obayashi, S., and Guruswamy, G.; “Navier-Stokes Computations for Oscillating Control Surfaces,” AIAA Paper No. 92-4431, August 1992.Google Scholar
  6. 6.
    Klopfer, G.H. and Molvik, G.A.; “Conservative Multizonal Interface Algorithm for the 3-D Navier-Stokes Equations,” AIAA Paper No. 91-1601CP, June 1991.Google Scholar
  7. 7.
    Chaussee, D.S. and Klopfer, G.H.; “The Numerical Study of 3-D Flow Past Control Surfaces,” AIAA Paper No. 92-4650, August 1992.Google Scholar

Copyright information

© Springer-Verlag 1995

Authors and Affiliations

  • G. H. Klopfer
    • 1
  • S. Obayashi
    • 1
  1. 1.MCAT InstituteNASA Ames Research CenterMofett Field

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