A Multi-GPU Parallel Algorithm in Hypersonic Flow Computations

Table 1

The flow conditions for the aerospace plane.

Case		[1/m]	[MPa]	[K]	[^0]
Case 1	8.02		6.0	740	0
Case 2	8.02		6.0	740	5
Case 3	10.02		6.9	1,457	0
Case 4	10.02		6.9	1,457	10