摘要: This paper represents an initial study on the use of quasi-static shape change devices in aircraft maneuvering. The macroscopic effects and requirements for these devices in flight control are the focus of this study. Groups of de... 展开
作者 | Montgomery, R. C. Scott, M. A. Weston, R. P. | ||
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原报告号 | N19980032587 | 总页数 | 14 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aircraft maneuvers Flight control Computational fluid dynamics Fighter aircraft Control equipment Leading edges Mach number Supersonic aircraft Simulation Stability Wings |