摘要: Wind tunnel investigations have been conducted of forebody strakes for yawcontrol on 0.06-scale models of the F/A-18 aircraft at free-stream Mach numbers
| 作者 | Erickson, G. E. Murri, D. G. | ||
|---|---|---|---|
| 原报告号 | N9416573 | 总页数 | 101 |
| 报告类别/文献类型 | NASA / NTIS科技报告 | ||
| 关键词 | Directional control F-18 aircraft Flow visualization Forebodies Strakes Subsonic speed Transonic speed Vortices Wind tunnel tests Yaw Aerodynamics Angle of attack Flow distribution Mach number Planforms Pressure distribution Static pressur | ||
