摘要: Wind tunnel tests were conducted in the Arnold Engineering Development Center (AEDC) Aerodynamic Wind Tunnel (4T) on a 0.06-scale model of the Minuteman Instrumented Payload Delivery System (MIPDS). Pressure distributions and forc... 展开
| 作者 | David M. Cahill | ||
|---|---|---|---|
| 原报告号 | ADB013389 | 总页数 | 106 |
| 主办者 | Arncld Engineering Development Center Air Force Systems Command | ||
| 报告类别/文献类型 | AD / NTIS科技报告 | ||
| 关键词 | Surface to surface missiles Instrumentation Pressure distribution Force(Mechanics) Moments Payload Payload analyses Mach number Angle of attack Minuteman Minuteman 3 missiles Supersonic characteristics Minuteman instrumented payload delivery system Nose cones Transonic characteristics Wind tunnel models Model tests Guided missile models | ||
