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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
@@ -57,10 +58,12 @@ ensures greater diversity than existing ones. Please refer to our [arXiv paper](
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  <img src="https://cdn-uploads.huggingface.co/production/uploads/6878e482bd4380c813fd99de/deWUNg0C2bxl7ZDQFfowu.png" alt="transform" width="40%">
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- 5. Raw solver output
 
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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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+
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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
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
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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
51
+ output for a machine learning model that predicts the aerodynamics of wings**.
52
 
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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
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
 
58
 
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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