摘要: Flight experiments were conducted to evaluate two control concepts for configuration management during the transition to landing approach for a powered-lift STOL aircraft. NASA Ames' augmentor wing research aircraft was used in th... 展开
作者 | Franklin, J. A. Innis, R. C. | ||
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原报告号 | N80-19127 | 总页数 | 32 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Approach Configuration management Controllability Powered lift aircraft Short takeoff aircraft Aircraft landing Airspeed Attitude control Flight paths Research aircraft Speed control |