摘要
A mixed Jameson/total-variation diminishing scheme applied to simulating rotor airfoil flowfield was presented. The scheme is used to solve the Euler equations for the simulation of the flowfield around a rotor airfoil. Considering the Euler equations' deficiency in reflecting viscous effects, Jameson's scheme was applied to solve the Navier-Stokes equations. Results of the calculation and experimental data were found in good agreement for Caradonna and Tung's rotor blades.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 213-216 |
| 页数 | 4 |
| 期刊 | Journal of Aircraft |
| 卷 | 40 |
| 期 | 1 |
| DOI | |
| 出版状态 | 已出版 - 2003 |
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