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Advances in Aerodynamics

Table 2 Computational parameters and mesh scales in NC case at x = 1000 mm

From: On the drag reduction mechanism of hypersonic turbulent boundary layers subject to heated wall blowing

Ma∞

Re∞/mm

(Lx, Ly, Lz)/mm

Nx, Ny, Nz

Δx+

Δyw+

Δz+

6

2.0 × 104

1310 × 36 × 30

4482 × 155 × 256

6.3

0.47

3.7

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