摘要: In 1993, tail buffet tests were performed on a full-scale, production model F/A-18 in the 80 x 120-foot Wind Tunnel at NASA Ames Research Center. Steady and unsteady pressures were recorded on both sides of the starboard vertical ... 展开
作者 | Moses, R. W. Pendleton, E. | ||
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原报告号 | N19970001676 | 总页数 | 16 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Pressure measurement Angle of attack Wind tunnel tests Bending moments Pressure distribution Tail assemblies Buffeting Full scale tests Scale models F-18 aircraft Free flow Sideslip Wind tunnel models Rudders Actuators Leading edges Trailing edges Data correlation Pressure oscillations Pressure sensors |