In this project, you'll find the full project details of a modal analysis of a typical aircraft wing. Below you'll notice that one end is fixed (as it would be to the fuselage). The same image also shows the mesh
The modes of the aluminum wing are:
| Mode | Frequency [Hz] |
|---|---|
| 1 | 4.83 |
| 2 | 25.32 |
| 3 | 32.17 |
| 4 | 38.08 |
| 5 | 48.30 |
| 6 | 53.53 |
The final results below indicate the total deformation at each mode.
- WorkBench 2020 R1 - CAE simulation framework used
- Ansys Mechanical APDL Solver - Modal analysis solving method
This project is licensed under the MIT License - see the LICENSE.md file for details