This repository is the implementation of the approach given by paper [1]. The vibration of the plate is solved by using a modified Ritz approach, where general boundary conditions are taken into account.

The implementation of the method is provided as the package plate. The data and figures in the paper are generated by python scripts starting with example in the project root and all the figures can be found in /figures.

To run the code, Python version >= 3.8 is required and additional packages such as numpy, scipy, matplotlib and sympy are also necessary.

[1] Ni Z, Li D, Ji L, et al. Aeroelastic modeling and analysis of honeycomb plates in high-speed airflow with acoustic load and general boundary conditions[J]. Composite Structures, 2023, 305: 116504.