Advances in Aerodynamics

Table 2 Parameters of CNN

From: Flow field reconstruction and shock train leading edge position detection of scramjet isolation section based on a small amount of CFD data

Layer	Input size	Kernel size	ReLU	Output size
Deconv1	1 × 2 × 10	2 × 2	Y	32 × 4 × 20
Deconv2	32 × 4 × 20	2 × 2	Y	16 × 8 × 40
Deconv3	16 × 8 × 40	2 × 2	Y	14 × 16 × 80
Deconv4	14 × 16 × 80	2 × 2	Y	10 × 32 × 160
Conv1	10 × 32 × 160	3 × 3	Y	8 × 16 × 80
Conv2	8 × 16 × 80	3 × 3	Y	20 × 8 × 40
Max pool	20 × 8 × 40	2 × 2	N	20 × 4 × 20
Conv3	20 × 4 × 20	3 × 3	Y	20 × 4 × 20
FC1	20 × 4 × 20	/	Y	6000
FC2	6000	/	N	10,500

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