Unsteady transonic aerodynamic loadings on the airfoil caused by heaving, pitching oscillations and control surface

Gao Zheng-hong

doi:10.1007/BF02481800

Unsteady transonic aerodynamic loadings on the airfoil caused by heaving, pitching oscillations and control surface

Gao Zheng-hong

航空学院

科研成果: 期刊稿件 › 文章 › 同行评审

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.

源语言	英语
页（从-至）	805-813
页数	9
期刊	Applied Mathematics and Mechanics (English Edition)
卷	13
期	9
DOI	https://doi.org/10.1007/BF02481800
出版状态	已出版 - 9月 1992

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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.",

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AB - 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.

KW - Euler equations

KW - heaving oscillation

KW - pitching oscillation

KW - transonic

KW - unsteady flow

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M3 - 文章

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ER -

Unsteady transonic aerodynamic loadings on the airfoil caused by heaving, pitching oscillations and control surface

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