摘要: The primary objective of structural analysis of aerospace applications is toobtain a verified finite element model (FEM). The verified FEM can be used for loads analysis, evaluate structural modifications, or design control system... 展开
作者 | Angelucci, F. Javeed, M. Mcgowan, P. | ||
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原报告号 | N9222279 | 总页数 | 112 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Dynamic tests Finite element method Mathematical models Structural analysis Trusses Correlation Nastran Aerospace engineering Computer programs Dynamic characteristics Loads (Forces) Modal response Software tools Structural design |