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. | ||
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原报告号 | AD9204272 | 总页数 | 77 |
主办者 | Non Paid Delimited ADS | ||
报告分类号 | [51C - Aircraft50 - Civil Engineering62A - Computer Hardware] | ||
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Sonic fatigue Airframes Thermal fatigue Airplane panels Computer programs Correlation techniques High temperature Dynamic response Curvature Structural response Nomographs Buckling Amplitude Thermal stresses Mathematical prediction Structural properties Compressive properties Bays(Structural units) Skin(Structural) Stiffness Subroutines Fortran Digital computers Aerothermoelasticity Aluminum alloys Titanium alloys Frequency response Vibration Thermal cycling tests Life expectancy Experimental data Unival 1106 computer Finite element method |