摘要: Stability and control characteristics of variable sweep airplane configuration capable of low-level supersonic attack - outer wing swept 75 degrees and 108 degrees
| 作者 | Howard, P. W. Robinson, R. B. | ||
|---|---|---|---|
| 原报告号 | NASA-TM-X-320 | 总页数 | 23 |
| 报告类别/文献类型 | NASA / NTIS科技报告 | ||
| 关键词 | ATTACK AIRCRAFT MACH NUMBER STABILITY SUPERSONIC AIRCRAFT SWEPT WINGS WINGS STABILITY AND CONTROL SUPERSONIC STRIKE AIRCRAFT SWEPT WING | ||
