摘要: A simulation experiment was conducted on Ames Research Center's Vertical MotionSimulator to evaluate the thrust margin for vertical landing required for the YAV-8B Harrier. Two different levels of ground effect were employed, repr... 展开
作者 | Franklin, J. A. Stortz, M. W. | ||
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原报告号 | N9411259 | 总页数 | 26 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Flight characteristics Ground effect (Aerodynamics) Harrier aircraft Stovlaircraft V/stol aircraft Vertical landing Vertical motion simulators Descent High temperature gases Hovering Inlet temperature Lift devices Temperature profiles Touchdo |