The Influence of Bleeding Direction on Starting Performance of Three-Dimensional Inward Turning Inlet

Table 1

Mesh validation results of hypersonic aerospace airplane.

Mesh type	Mesh number
Coarse mesh	2.49 million	-6.0708-02	4.3184-03
Medium mesh	4.27 million	-6.1041-02	6.1150-03
Fine mesh	6.48 million	-6.0979-02	5.0931-03