A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures.
The design of structures submitted to aerodynamic loads usually requires the development of specific computational models considering fluid-structure interactions. Models using structural frame elements are developed in several relevant applications such as, the design of advanced aircraft wings, wi...
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| Format: | article |
| Language: | English |
| Published: |
2023
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| Online Access: | https://hdl.handle.net/20.500.12008/41731 |
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