抄録
A two-dimensional blunt body was submerged in a compressible turbulent boundary layer and the surface pressure was measured. It was found the fore-body drag was reduced due to the velocity defect in the boundary layer and the associated re-circulation behind an oblique shock wave. A small two-dimensional shock generator ahead of the blunt body further reduced the drag of the blunt body.
| 本文言語 | 英語 |
|---|---|
| ページ（範囲） | 474-476 |
| ジャーナル | Transactions of the Japan Society for Aeronautical and Space Sciences |
| 巻 | 50 |
| 号 | 586 |
| 出版ステータス | 出版済み - 2002 |