摘要: A wind-tunnel test was conducted at Ames Research Center to measure the aerodynamic characteristics of a joined-wing research aircraft (JWRA). This aircraft was designed to utilize the fuselage and engines of the existing NASA AD-... 展开
作者 | Smith, S. C. Stonum, R. K. | ||
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原报告号 | N8924285 | 总页数 | 100 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aircraft stability Joined wings Leading edges Wind tunnel tests Ailerons Aircraft control Aircraft models Aircraft performance Angle of attack Control surfaces Lateral stability Longitudinal stability Mach number Reynolds number Sideslip |