Program

1.  Material Definition:

          Define the composite material by specifying the elastic modulus, shear modulus, and Poisson’s ratio.

2.  Layer Configuration:

         Specify the material, stacking angle, and thickness to define a laminate layer.

3.  Composite Properties:

         Stack the laminate by selecting the defined layer, and then calculate the ABD matrix and engineering constants.

4.  Buckling Pressure:

         Calculate buckling pressure under external loads using defined geometric properties and design codes (ASME and NASA).

1.  CFD Results Input:

         Define the spatial and temperature data. The required input data should be formatted as a .csv file.

2. Regression Analysis:

        Conduct Random Forest regression to derive a new temperature profile suitable for the finite element model. 

        This step also includes generating a regression plot to display the accuracy of the Random Forest model.

3. Write the FE Files: 

        Automatically generate the temperature profile and coordinate point information into an LS-DYNA code file (.k).

        This process necessitates the coordinate point dataset from the FE model and incorporates time step information.

1. Input and calculation: 

Define the spatial and heat flux data. By entering some values such as initial timestep, exposure time, and clothes factor,      the result of POI can be generated.

2. Plotting: 

A 3D graph displays the POI in each coordinate point. A prompt is provided to select the degree of burns.