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THE STUDY OF FLOW OVER OSCILLATING AIRFOILS AND AIRFOILS WITH TRAILING-EDGE FLAP[J]. Chinese Journal of Theoretical and Applied Mechanics, 1993, 25(1): 1-7. DOI: 10.6052/0459-1879-1993-1-1995-607
Citation: THE STUDY OF FLOW OVER OSCILLATING AIRFOILS AND AIRFOILS WITH TRAILING-EDGE FLAP[J]. Chinese Journal of Theoretical and Applied Mechanics, 1993, 25(1): 1-7. DOI: 10.6052/0459-1879-1993-1-1995-607
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THE STUDY OF FLOW OVER OSCILLATING AIRFOILS AND AIRFOILS WITH TRAILING-EDGE FLAP

  • 北京空气动力研究所,100074

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  • The dynamic precess was numerically simulated on a two dimensional oscillating airfoil or an airfoil with trailing-edge flap in pitch. The Euler and Navier-Stokes equations with Baldwin-Lomax turbulent model were required to solve using the implicit fac-torized finite difference algorithm(LU-AD1 algorithm), which was constructed n a body fitted coordinate system. The study was focused on the unsteady effect of shock wave and control of separation on the lifting surface due to the oscillation. The numerical ...
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