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- W2386439942 abstract "With the broad usage of composite in newly aviation structure,the engineering aeroelastic modeling and analysis of composite wing are important project to aircraft design.By the aeroelasticity theory and method,structure model with FEM,model correction,natural vibration calculation,flutter analysis were made.Based on the static analysis model,structure drawing and relating test results,the model was modified iteratively to get rational dynamic model.Using MSC/NASTRAN,the dynamic reduction method was applied to avoid local modes and promote the prices.The flutter analysis for the wing was made with the unsteady aerodynamic which was solved by subsonic double lattice method." @default.
- W2386439942 created "2016-06-24" @default.
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- W2386439942 date "2007-01-01" @default.
- W2386439942 modified "2023-09-28" @default.
- W2386439942 title "Study of Aeroelasticity for Composite Wing with High-aspect-ratio" @default.
- W2386439942 hasPublicationYear "2007" @default.
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