Structural Optimization of the Aircraft NACA Inlet Based on BP Neural Networks and Genetic Algorithms

Table 2

Comparisons between predictions of CFX and test results.

Method
Experiment	0.500	0.02950	—
Simulation calculation (grid number 6353702)	0.500	0.03094	0.000144
Simulation calculation (grid number 10694138)	0.500	0.029781	0.00031
Simulation calculation (grid number 19745870)	0.500	0.02976	0.00026
Simulation calculation (grid number 29573892)	0.500	0.02975	0.00025