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README.md
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# AIAA Applied Aerodynamics Surrogate Modeling - Case 4
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This folder contains the data available for the AIAA Applied Surrogate Modeling
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benchmark case 4 which consists out of in total 149 surface solutions solving
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the RANS equations. The corresponding AIAA SciTech2025 Paper provides more
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information about the dataset.
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The data is split in training and test samples in separat folders. All are
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available in two hdf5 files, one for training samples and one for test samples.
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These files provide parameter information (Mach, AoA, innerAileron,
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outerAileron, htp angle and elevator) and surface values (cp, cf, coords,
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normals, surface areas). An additional file is available providing connectivity
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information.
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Note that, if validation data is needed for your surrogate modeling technique
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these should be taken from the training samples.
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In addition to the data a simple python script *h5Import_NASA-CRM.py* is
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available. This file provides a function which reads the data from h5 file. It
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returns a dictionary with the sample numbers as keys. Under each key another
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dictionary is available with global informations such as parameters values and
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global coefficients and surface solutions as numpy arrays.
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