An effective computer modelling approach to the study of aeroelastic characteristics of an aircraft composite wing with high aspect ratio (Q5248057)
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scientific article; zbMATH DE number 6431160
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | An effective computer modelling approach to the study of aeroelastic characteristics of an aircraft composite wing with high aspect ratio |
scientific article; zbMATH DE number 6431160 |
Statements
An effective computer modelling approach to the study of aeroelastic characteristics of an aircraft composite wing with high aspect ratio (English)
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27 April 2015
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honeycomb core sandwich composite
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high-aspect ratio wing
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stiffness distribution
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static aeroelasticity
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flutter
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CFD/CSD coupled method
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