| タイトル | Research on the sonic boom problem. Part 2: Flow field measurement in wind tunnel and calculation of second order F-function |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740001919 |
| 著者（英） | Soerensen, H.; Landahl, M.; Hilding, L. |
| 著者所属（英） | Aeronautical Research Inst. of Sweden |
| 発行日 | 1973-11-01 |
| 言語 | eng |
| 内容記述 | An experimental investigation has been carried out in a wind tunnel to test some of the results of Landahl's second order theory. The slender models consisted of a parabolic spindle, tested at M = 3, and a wing body configuration, suggested by Ferri, and tested at M = 2.7. The theory indicates that shock position and strength at an arbitrary distance can be calculated by means of near field measurements. The results show that this method is an appropriate one for simple bodies and for bodies with complicated geometries as well. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 74N10031
NASA-CR-2340
FFA-AU-621-PT-2 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/197102 |
