摘要: Experimental longitudinal and lateral-directional aerodynamic characteristics were obtained for the Pegasus and Pegasus XL configurations over a Mach number range from 1.6 to 6 and angles of attack from -4 to +24 degrees. Angle of... 展开
作者 | Rhode, M. N. Engelund, W. C. Mendenhall, M. R. | ||
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原报告号 | N19970013282 | 总页数 | 22 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Pegasus air-launched booster Aerodynamic characteristics Angle of attack Mach number Ailerons Directional stability Flight tests Directional control Lateral control Lateral stability Sideslip Flight characteristics Controllability Separated flow Elevons Rudders Tail assemblies |