科技报告详细信息
| Passive Aeroelastic Tailored Wing Ground Vibration Test Using Fixed Base Correction Method | |
| Spivey, Natalie | |
| 关键词: ACCELEROMETERS; AERODYNAMIC LOADS; AEROELASTICITY; AIRCRAFT DESIGN; CORRECTION; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; RETRACTABLE EQUIPMENT; TEST FACILITIES; WING LOADING; WINGS; | |
| RP-ID : AFRC-E-DAA-TN69491 | |
| 学科分类：力学，机械学 | |
| 美国|英语 | |
| 来源: NASA Technical Reports Server | |
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【 预 览 】
| Files | Size | Format | View |
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| 20190026540.pdf | 4298KB |  download |
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