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- W2247228941 abstract "This paper is a study on the coupled load analysis using MSC/Nastran superelement method, After selecting the launch vehicle, coupled load analysis is performed. From the results of coupled load analysis, the loads and displacements on the major parts of satellite structure are calculated, Based on theses loads and displacements, the safety of satellite structure is judged. Coupled load analysis has been executed using MSC/Nastran DMAP code so far. Because DMAP code was very complicated and long in length, it was difficult to analyze and modify the DMAP code. To solve out these problems, coupled load analysis was executed using M3C/Nastran 2005 superelement method, At first, satellite FE-model was converted to the Craig-Hampton model using MSC/Nastran 2005 superelement method and verified. Finally, coupled load analysis was performed using satellite Craig-Hampton model and launch vehicle FE-model and verified." @default.
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- W2247228941 date "2006-11-01" @default.
- W2247228941 modified "2023-09-23" @default.
- W2247228941 title "MSC/Nastran Superelement를 이용한 연성하중해석" @default.
- W2247228941 hasPublicationYear "2006" @default.
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