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)


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