摘要: A wind tunnel test was conducted to obtain the surface pressure distributions of three elliptic missile body configurations. The test was performed at nominal Mach numbers from 0.4 to 1.3 at a constant nominal free-stream unit Rey... 展开
作者 | Sellers, M. E. | ||
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原报告号 | ADA166552 | 总页数 | 39 |
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Guided missile models Aerodynamic configurations Subsonic characteristics Transonic characteristics Supersonic characteristics Angle of attack Angles Ellipses Free stream Experimental data Power Pressure Pressure distribution Range(Extremes) Reynolds nu |