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Advances in Aerodynamics

Table 2 The test cases for the Shenzhou reentry capsule

From: DSMC modeling of rarefied ionization reactions and applications to hypervelocity spacecraft reentry flows

Case

M∞

P0(MPa)

T0(K)

Kn∞(× 10− 2)

1

12.98

1.309

595

1.81

2

12.90

0.662

597

2.59

3

12.69

0.280

595

3.73

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