摘要: The purpose is to determine the tailless aircraft performance improvements gained from relaxed static stability, to quantify this potential in terms of range-payload improvements, and to identify other possible operational and han... 展开
作者 | Ashkenas, I. L. Klyde, D. H. | ||
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原报告号 | N8920999 | 总页数 | 145 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aircraft control Aircraft performance Remotely piloted vehicles Static stability Tail assemblies Aircraft configurations Ailerons High aspect ratio Improvement Landing Takeoff Trailing edges Wings Yaw |