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Advances in Aerodynamics

Table 1 The upstream condition, the stagnation pressure and the reservoir pressure

From: Numerical investigation of an active TPS for a wing leading edge exposed to high temperature air behind a strong bow shock wave

 

M∞

Re∞

T∞ [K]

P∞ [Pa]

Psta [Pa]

Pres [Pa]

Case-A

5

460,000

230

1000

3.26E+ 4

3.29E+ 4

Case-B

27

2600

200

1

9.44E+ 2

1.20E+ 3

Case-C

7.5

34,000

270

76

5.54E+ 3

5.85E+ 3

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