| タイトル | A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810005404 |
| 著者（英） | Ashby, G. C., Jr. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1980-12-01 |
| 言語 | eng |
| 内容記述 | An experimental and analytical study of the sonic boom static pressure signatures generated by a blunt body at mach 6 has shown that finite difference computer programs can be used to give reasonable estimates of the signatures. The calculated near field static pressure signature was extrapolated to the far field by a program using the method of characteristics. A comparison of this extrapolated signature with the signature predicted by far field sonic boom theory (linearized) shows that peak overpressures are about the same, at least up to mach, but the far field theory overestimates the length of the signature. |
| NASA分類 | AERONAUTICS (GENERAL) |
| レポートNO | 81N13915
NASA-TP-1787
L-14017 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/170532 |
