摘要: Wind-tunnel studies have been performed in the Langley Hypersonic Helium Tunnel Facility to obtain static longitudinal and lateral-directional aerodynamic characteristics of an advanced aerospace plane concept. The nominal test co... 展开
作者 | Mccandless, R. S. | ||
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原报告号 | N8615245 | 总页数 | 28 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Angle of attack Hypersonic wind tunnels Lateral stability Longitudinal stability Sideslip Static loads Helium Mach number Reynolds number Aerodynamic characteristics Canopies Elevators (Control surfaces) Elevons Rudders Wind tunnel tests |