摘要: An aid in airplane design, charts have been prepared to show the effects of wing taper, thickness ratio, and Reynolds number on the spanwise location of the initial stalling point. Means of improving poor stalling characteristics ... 展开
作者 | Soule, H A Anderson, R F | ||
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原报告号 | NACA-TR-703 | 总页数 | 11 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | SWEPT WINGS AERODYNAMIC STALLING AIRCRAFT DESIGN COMPUTATION WING PROFILES THICKNESS RATIO REYNOLDS NUMBER AERODYNAMIC DRAG DESIGN CHARTS |