摘要: The investigation reported herein was conducted on a transonic bump to determine the aerodynamic characteristics of a series of triangular wings. Four basic triangular-wing plan forms having aspect ratios of 2.0, 2.5, 3.0, and 4.0... 展开
作者 | Emerson, H. F. | ||
---|---|---|---|
原报告号 | ADA377454 | 总页数 | 187 |
主办者 | Non Paid ADAS | ||
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Aerodynamic characteristics Wind tunnel tests Wing tips Ratios Thickness Taper Mach number Range(Extremes) Drag Wings Test facilities Reynolds number Aspect ratio Camber Triangular wings Transonic bump method |