科技报告详细信息
| PAT Wing Fixed Base Correction Modal Testing Debrief | |
| Napolitano, Kevin ; Spivey, Natalie ; Miller, Kia | |
| 关键词: AEROELASTIC RESEARCH WINGS; GROUND TESTS; FREQUENCY RESPONSE; MODAL RESPONSE; CORRECTION; SHAKERS; FLUTTER; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; STRUCTURAL DESIGN; NASA PROGRAMS; | |
| RP-ID : AFRC-E-DAA-TN60636 | |
| 美国|英语 | |
| 来源: NASA Technical Reports Server | |
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【 摘 要 】
This presentation is an overview of the PAT (Passive Aeroelastic Tailored) Wing ground vibration test and the fixed-base correction research being performed here.
【 预 览 】
| Files | Size | Format | View |
|---|---|---|---|
| 20180006673.pdf | 3488KB |  download |
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