Table 4 Summary of absolute and relative error of \({C}_{D}\) and \({C}_{L}\) coefficients predicted by the CNN.
From: CNN-based flow control device modelling on aerodynamic airfoils
Error | \({C}_{D}\) | \({C}_{L}\) | ||||
|---|---|---|---|---|---|---|
Min | Max | Mean | Min | Max | Mean | |
Absolute error | 0.00002 | 0.00074 | 0.00023 | 0.0005 | 0.04 | 0.0089 |
Relative error | 0.19% | 32.44% | 6.17% | 0.033% | 2.786% | 0.827% |
