| タイトル | Subsonic longitudinal aerodynamic characteristics and engine pressure distributions for an aircraft with an integrated scramjet designed for Mach 6 cruise |
| 本文（外部サイト） | http://hdl.handle.net/2060/19770026164 |
| 著者（英） | Huffman, J. K.; Johnston, P. J.; Fox, C. H., Jr. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1977-08-01 |
| 言語 | eng |
| 内容記述 | A 1/10-scale model of a proposed hypersonic aircraft with an integrated scramjet was tested. The investigation took place over a Mach number range from 0.2 to 0.7 and an angle of attack range from 2 deg to approximately 17 deg at a sideslip angle of 0 deg. The primary configuration variables studied were engine location, internal engine geometry, and external engine geometry. The results are presented without analysis. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 77N33108
NASA-TM-X-73911 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/181135 |
