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.
| Original language | English |
|---|---|
| Pages (from-to) | 805-813 |
| Number of pages | 9 |
| Journal | Applied Mathematics and Mechanics (English Edition) |
| Volume | 13 |
| Issue number | 9 |
| DOIs | |
| State | Published - Sep 1992 |
Keywords
- Euler equations
- heaving oscillation
- pitching oscillation
- transonic
- unsteady flow
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