摘要: The unsteady pressures acting on the vertical tails of a full-scale F/A-18 fighter aircraft were studied to gain a better understanding of tail-buffet loads that frequently occur on fighter aircraft operating at high angles-of-att... 展开
作者 | Meyn, L. A. James, K. D. | ||
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原报告号 | N20010062152 | 总页数 | 10 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aerodynamic loads Tail assemblies Angle of attack F-18 aircraft Stabilizers(Fluid dynamics) Bending moments Leading edges Loads(Forces) Unsteady aerodynamics Pressure sensors Wind tunnels |