| タイトル | Methodology for matching experimental and computational aerodynamic data |
| 本文（外部サイト） | http://hdl.handle.net/2060/19880014344 |
| 著者（英） | Wieseman, Carol D. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1988-05-01 |
| 言語 | eng |
| 内容記述 | Correction factor methodologies have been developed which use steady experimental or analytical pressure or force data to correct steady and unsteady aerodynamic calculations. Three methods of calculating correction factors have been developed to match steady surface pressure distributions, to match airfoil section forces and moments. Data for a rectangular supercritical wing that was previously tested in the NASA Langley Research Center Transonic Dynamics Tunnel have been used to determine correction factors to match surface pressure distributions for a range of Mach numbers. |
| NASA分類 | AERONAUTICS (GENERAL) |
| レポートNO | 88N23728
NASA-TM-100592
AIAA PAPER 88-2392
NAS 1.15:100592 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/146235 |
