Numerical Analysis and Experimental Techniques for Static Aeroelastic Divergence of Wing
Aeroelastic divergence analysis of a stable wing structure was performed using a coupled aerodynamic/structural method and validated using wind tunnel tests. To ensure the accuracy of numerical analysis, CFD method was used for aerodynamic force calculation and finite element method was used for str...
| मुख्य लेखकों: | , , |
|---|---|
| स्वरूप: | लेख |
| भाषा: | zho |
| प्रकाशित: |
China Astronautic Publishing CO., LTD. ; Editorial Office of Physics of Gases
2023-11-01
|
| श्रृंखला: | 气体物理 |
| विषय: | |
| ऑनलाइन पहुंच: | http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.1087 |