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Table 3 The inclination angles of the high-frequency pw (αp) and those of the wall parallel velocity components at the edge of the boundary layer (αe) and the first layer of grid (αw)

From: Wall pressure beneath a transitional hypersonic boundary layer over an inclined straight circular cone

Group 1 A B C D E F G
αe () 1.01 2.32 3.39 4.29 5.49 5.87 6.62
αw () 4.33 9.17 13.56 17.29 22.48 24.37 28.07
αp () 1.0 3.0 8.0 10.0 15.0 15.0 3.0
Group 2 A’ B’ C’ D’ E’ F’  
αe () 4.46 4.98 6.17 6.43 6.94 7.06  
αw () 15.80 19.45 22.95 23.40 24.30 11.87  
αp () 10.0 10.0 12.0 15.0 15.0 8