摘要: An analytical and experimental program was conducted to develop acoustic fatigue design criteria for aircraft structures subjected to intense noise in a high temperature environment. Equations for the dynamic response of a buckled... 展开
| 作者 | Schneider, C. W. | ||
|---|---|---|---|
| 原报告号 | AD9202821 | 总页数 | 217 |
| 主办者 | Non Paid Delimited ADS | ||
| 报告分类号 | [46E - Structural Mechanics51C - Aircraft50 - Civil Engineering] | ||
| 报告类别/文献类型 | AD / NTIS科技报告 | ||
| 关键词 | Sonic fatigue Airframes Thermal fatigue Airplane panels Structural response Buckling Dynamic response Mathematical prediction Bays(Structural units) Experimental data Correlation techniques Mathematical models Structural properties Curvature Structural members Computer programs Skin(Structural) Stiffness Thermal stresses Strain(Mechanics) Aluminum alloys Titanium alloys Frequency response Vibration Stiffening Flanges Surface temperature Life expectancy Degradation Numerical analysis Test methods Confidence level Nomographs High temperature Dynamic structural analysis Structural design Design Fatigue tests Stiffened panels Substructures Structural analysis Stress analysis | ||
