| タイトル | The Jacobi Matrix Technique in Computational Fluid Dynamics |
| 本文（外部サイト） | http://hdl.handle.net/2060/19870018915 |
| 著者（英） | Sharp, H. Thomas |
| 著者所属（英） | Brown Univ. |
| 発行日 | 1988-05-01 |
| 言語 | eng |
| 内容記述 | The Jacobi matrix technique was applied to the direct calculation of inviscid supersonic flow about two dimensional airfoils of varying thickness, angle of attack and camber and axisymmetric bodies of varying thickness and taper; and the design (inverse) calculation of inviscid supersonic flow past airfoils described by a given family of pressure distributions and axisymmetric bodies described by a given family of pressure distributions. The method was also applied to subsonic potential flow about two dimensional airfoils by modifying Jameson's FLO36. Results are discussed. |
| NASA分類 | NUMERICAL ANALYSIS |
| レポートNO | 87N28348
N87-28348 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/149089 |
|
