Unsteady Transonic Aerodynamic Loadings on the Airfoil Caused by Heaving, Pitching Oscillations and Control Surface

Gao Zheng-hong

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Article Navigation > Applied Mathematics and Mechanics > 1992 > 13(9): 775-783

Gao Zheng-hong. Unsteady Transonic Aerodynamic Loadings on the Airfoil Caused by Heaving, Pitching Oscillations and Control Surface[J]. Applied Mathematics and Mechanics, 1992, 13(9): 775-783.

Citation:

Gao Zheng-hong. Unsteady Transonic Aerodynamic Loadings on the Airfoil Caused by Heaving, Pitching Oscillations and Control Surface[J]. Applied Mathematics and Mechanics, 1992, 13(9): 775-783.

Citation:

Gao Zheng-hong. Unsteady Transonic Aerodynamic Loadings on the Airfoil Caused by Heaving, Pitching Oscillations and Control Surface[J]. Applied Mathematics and Mechanics, 1992, 13(9): 775-783.

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Unsteady Transonic Aerodynamic Loadings on the Airfoil Caused by Heaving, Pitching Oscillations and Control Surface

Gao Zheng-hong

Northwestern Polytcchnical University, Xi'an

Received Date: 1991-06-09
Publish Date: 1992-09-15

Abstract

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.
- transonic,
- unsteady flow,
- Euler equations,
- heaving oscillation

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References(11)

References

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