Experimental Investigation of Brazilian 14-X B Hypersonic Scramjet Aerospace Vehicle

Table 2

Thermodynamic properties of the airflow field along the 14-X B model lower surface considering the freestream properties for real gas simulation, power-off case, inviscid flow, and .

Quantity	Unit	Inlet entrance	1st ramp	2nd ramp	Combustor entrance	Internal expansion surface	External expansion surface
		7.10	7.10	6.18	4.14	2.68	2.88
	°		5.00	14.5	19.5	4.27	10.73
	°		11.088	21.377	30.793
			6.183	4.140	2.676	2,879	3.473
	K	227,00	290,92	568.23	1,034.30	946.49	737.18
	Pa	1,818.00	4,103.93	24,797.37	130,604.94	95,742.29	39,921.56
	kg/m^3	0.0279	0.0492	0.1521	0.4400	0.3525	0.1887
	m/s	302.01	341.90	477.82	644.66	616.68	544.24
	m/s	2,144.25	2,114.10	1,977.95	1,725.10	1,775.49	1,890.20