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

Table 1

Structure parameters.

Throat aspect ratio	Slope inclination (°)	Opening length (mm)
2	6	1460
2.4	6.4	1555
2.8	6.8	1650
3.2	7.2	1745
3.6	7.6	1840
4	8	1935