DSMC Simulation and Experimental Validation of Shock Interaction in Hypersonic Low Density Flow

Table 1

Test case in [1].

Run	𝑉∞ (m/s)	𝜌∞ (Kg/m^3 ×10^3)	𝑃∞ (Pa)	Ma	Re/m (×10^5)	Nose
26	2581	1.093	48.7	10.34	1.704	Sharp
28	2520	0.727	30.0	10.50	1.106	Sharp
35	2575	0.608	18.5	12.49	0.945	Sharp
32	2572	0.758	32.1	10.56	1.177	R0.250
33	2636	1.288	59.8	10.35	2.050	R0.250
36	2584	1.108	49.6	10.34	1.729	R0.250
38	2453	0.498	13.9	12.47	0.738	R0.288