Applied Mathematics and Mechanics (English Edition) ›› 1992, Vol. 13 ›› Issue (9): 805-813.

• 论文 • 上一篇    下一篇

UNSTEADY TRANSONIC AERODYNAMIC LOADINGS ON THE AIRFOIL CAUSED BY HEAVING, PITCHING OSCILLATIONS AND CONTROL SURFACE

高正红   

  1. Northwestern Polytcchnical University, Xi’an
  • 收稿日期:1991-06-09 出版日期:1992-09-18 发布日期:1992-09-18

UNSTEADY TRANSONIC AERODYNAMIC LOADINGS ON THE AIRFOIL CAUSED BY HEAVING, PITCHING OSCILLATIONS AND CONTROL SURFACE

Gao Zheng-hong   

  1. Northwestern Polytcchnical University, Xi’an
  • Received:1991-06-09 Online:1992-09-18 Published:1992-09-18

摘要: An implicit upwind finite volume solver for the Euler equations using the improved flux-splitting method is established and used to calculate the transonic flow past the airfoils with heaving, pitching oscillations and the control surface. Results are given for the NACA64A-10 airfoil which is in harmonic heaving and pitching oscillation and with the control surface in the transonic flow field. Some computational results are compared with the experiment data and the good agreements are shown in the paper.

关键词: transonic, unsteady flow, Euler equations, heaving oscillation, pitching oscillation

Abstract: An implicit upwind finite volume solver for the Euler equations using the improved flux-splitting method is established and used to calculate the transonic flow past the airfoils with heaving, pitching oscillations and the control surface. Results are given for the NACA64A-10 airfoil which is in harmonic heaving and pitching oscillation and with the control surface in the transonic flow field. Some computational results are compared with the experiment data and the good agreements are shown in the paper.

Key words: transonic, unsteady flow, Euler equations, heaving oscillation, pitching oscillation

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