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Table 1 The flow conditions for the four additional test cases

From: The shape of incident shock wave in steady axisymmetric conical Mach reflection

 

Case I (Fig. 4)

Case II (Fig. 5)

Case III (Fig. 6)

Case IV (Fig. 7)

θw

10o

12 o

12 o

12 o

M∞

1.8

2.0

2.2

3.5

w/r0

0.6

0.6

0.6

0.6