Update README.md
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README.md
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@@ -44,10 +44,11 @@ ensures greater diversity than existing ones. Please refer to our [arXiv paper](
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|8|pitching moment coefficient|
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3. Reference surface mesh and surface physical quantities on this reference mesh
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The reference mesh `geom0` contains the cell-centric coordinates of the reference surface mesh with size \\( 256 \times 128 \times 3 \\), and the three channels stand
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for \\( x, y, z \\). The surface physical quantities `data.npy` are on the same reference mesh with size \\( 256 \times 128 \times 3 \\), and the three channels stand for
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\\( C_p, C_{f,\tau}, C_{f,z} \\). (the latter two are the decomposed friction coefficients on the streamwise and spanwise directions). These data can serve as input and
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output for a machine learning model that predicts the aerodynamics of wings
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**reference mesh**: The simulation mesh on the wing surface is first interpolated to a reference mesh. In the spanwise ($j$-direction), 128 cross-sectional planes are
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sampled with even spacing, and tips are excluded. For each cross-section (i-direction), a fixed set of normalized chordwise positions \\( \{(x/c)_i\} \\) s is used for both
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<img src="https://cdn-uploads.huggingface.co/production/uploads/6878e482bd4380c813fd99de/deWUNg0C2bxl7ZDQFfowu.png" alt="transform" width="40%">
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The raw output of surface flow (`surf.cgns`) and 3D volume fields (`vol.cgns`) is also available in their original formats (CGNS files with the ADF format). They need the
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CGNS library to be read out. Since they are too large, they are available via university storage upon reasonable request to the authors.
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The table below summarizes the data.
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|Type | File & Description | Size
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|8|pitching moment coefficient|
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3. Reference surface mesh and surface physical quantities on this reference mesh
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| 47 |
+
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| 48 |
The reference mesh `geom0` contains the cell-centric coordinates of the reference surface mesh with size \\( 256 \times 128 \times 3 \\), and the three channels stand
|
| 49 |
for \\( x, y, z \\). The surface physical quantities `data.npy` are on the same reference mesh with size \\( 256 \times 128 \times 3 \\), and the three channels stand for
|
| 50 |
+
\\( C_p, C_{f,\tau}, C_{f,z} \\). (the latter two are the decomposed friction coefficients on the streamwise and spanwise directions). **These data can serve as input and
|
| 51 |
+
output for a machine learning model that predicts the aerodynamics of wings**.
|
| 52 |
|
| 53 |
**reference mesh**: The simulation mesh on the wing surface is first interpolated to a reference mesh. In the spanwise ($j$-direction), 128 cross-sectional planes are
|
| 54 |
sampled with even spacing, and tips are excluded. For each cross-section (i-direction), a fixed set of normalized chordwise positions \\( \{(x/c)_i\} \\) s is used for both
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<img src="https://cdn-uploads.huggingface.co/production/uploads/6878e482bd4380c813fd99de/deWUNg0C2bxl7ZDQFfowu.png" alt="transform" width="40%">
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4. Raw solver output
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+
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The raw output of surface flow (`surf.cgns`) and 3D volume fields (`vol.cgns`) is also available in their original formats (CGNS files with the ADF format). They need the
|
| 64 |
CGNS library to be read out. Since they are too large, they are available via university storage upon reasonable request to the authors.
|
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+
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The table below summarizes the data.
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|Type | File & Description | Size
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