摘要: Report presents the results of flight tests comparing the relative effectiveness of conventional ailerons of the same size on wings of rectangular and tapered plan forms made with a Fairchild 22 airplane. Information is included c... 展开
作者 | Soule, H A Gracey, W | ||
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原报告号 | NACA-TR-630 | 总页数 | 5 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | AILERONS RECTANGULAR WINGS SWEPT WINGS AERODYNAMIC CHARACTERISTICS COMPUTATIONAL FLUID DYNAMICS FLIGHT TESTS COMPARISON WING TIPS FLOATING LATERAL CONTROL ROLLING MOMENTS |