摘要: An analysis is presented of the vertical-tail loads to be expected as a result of abrupt aileron action in accelerated flight, as in rolls from turns or pull-outs, for example. The formulas derived show that the vertical- tail loa... 展开
原报告号 | ADA801519 | 总页数 | 8 |
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主办者 | Non Paid ADAS | ||
报告分类号 | [51C - Aircraft, 51A - Aerodynamics] | ||
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Aerodynamic characteristics Loads(Forces) Ailerons Aircraft Dynamic loads Maneuvers Roll Stability Tail assemblies Wings Yaw Ati-13374 Ati collection |