| タイトル | Sonic Boom Minimization Efforts on Boeing HSCT Baseline |
| 著者（英） | Tu, Eugene; Fouladi, Kamran; Haglund, George; Cheung, Samson H. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1999-12-01 |
| 言語 | eng |
| 内容記述 | A team was formed to tackle the sonic boom softening issues of the current Boeing HSCT design. The team consisted of personnel from NASA Ames, NASA Langley, and Boeing company. The work described in this paper was done when the first author was at NASA Ames Research Center. This paper presents the sonic boom softening work on two Boeing High Speed Civil Transport (HSCT) baseline configurations, Reference-H and Boeing-1122. This presentation can be divided into two parts: parametric studies and sonic boom minimization by CFD optimization routines. |
| NASA分類 | Aerodynamics |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/539249 |
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