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UNSTEADY TRANSONIC AERODYNAMIC LOADINGS ON THE AIRFOIL CAUSED BY HEAVING, PITCHING OSCILLATIONS AND CONTROL SURFACE
作者姓名:高正红
作者单位:Northwestern Polytechnical
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.

收稿时间:9 June 1991

Unsteady transonic aerodynamic loadings on the airfoil caused by heaving,pitching oscillations and control surface
Gao Zheng-hong.UNSTEADY TRANSONIC AERODYNAMIC LOADINGS ON THE AIRFOIL CAUSED BY HEAVING, PITCHING OSCILLATIONS AND CONTROL SURFACE[J].Applied Mathematics and Mechanics(English Edition),1992,13(9):805-813.
Authors:Gao Zheng-hong
Institution:(1) Northwestern Polytechnical University, Xi'an
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.
Keywords:transonic  unsteady flow  Euler equations  heaving oscillation  pitching oscillation
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