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

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

Group 1

A

B

C

D

E

F

G

ιe (∘)

1.01

2.32

3.39

4.29

5.49

5.87

6.62

ιw (∘)

4.33

9.17

13.56

17.29

22.48

24.37

28.07

ιp (∘)

1.0

3.0

8.0

10.0

15.0

15.0

3.0

Group 2

A’

B’

C’

D’

E’

F’

 

ιe (∘)

4.46

4.98

6.17

6.43

6.94

7.06

 

ιw (∘)

15.80

19.45

22.95

23.40

24.30

11.87

 

ιp (∘)

10.0

10.0

12.0

15.0

15.0

8