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...
Saved in:
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | article |
| Language: | English |
| Published: |
2023
|
| Subjects: | |
| Online Access: | https://hdl.handle.net/20.500.12008/41731 |
| Tags: |
No Tags, Be the first to tag this record!
|
Similar Items: A co-rotational formulation for quasi-steady aerodynamic nonlinear analysis of frame structures.
- Analysis and Prediction of Heat Induced Deformation Produced By the Line Heating Process Using the Finite Element Method
- Effect of phase transformation onset temperature on residual stress in welded thin steel plates
- Robust Cascade Controller for Nonlinearly Actuated Biped Robots: Experimental Evaluation
- Finite element algorithms for nonlocal minimal graphs
- Acciones quasi conformes en superficies
- Analysis and prediction of welding distortion in complex structures using elastic finite element method