Table 3 Arithmetic mean and standard deviation of the results obtained by CFD and CNN.
From: CNN-based flow control device modelling on aerodynamic airfoils
Method | CFD | CNN | ||||
|---|---|---|---|---|---|---|
\({u}_{x}\) | \({u}_{y}\) | \(p\) | \({u}_{x}\) | \({u}_{y}\) | \(p\) | |
Arithmetic mean (µ) | 20.9538 | −2.5385 | 82.8164 | 20.9784 | −2.5076 | 82.9625 |
Standard deviation (σ) | 8.7620 | 2.0860 | 91.6118 | 8.7086 | 2.0939 | 90.7867 |
