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Passive Aeroelastic Tailored Wing Ground Vibration Test Using Fixed Base Correction Method.
| 题名： | Passive Aeroelastic Tailored Wing Ground Vibration Test Using Fixed Base Correction Method. |
| 作者： | Spivey, N. |
| 关键词： | Accelerometers, Aerodynamic loads, Wings, Aeroelasticity, Aircraft design, Correction, Finite element method, Mathematical models, Retractable equipment, Test facilities, Wing loading |
| 摘要： | No abstract available |
| 报告类型： | 科技报告 |
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