Design of a Three-Dimensional Hypersonic Inward-Turning Inlet with Tri-Ducts for Combined Cycle Engines

Table 4

Mass-averaged performance of the tri-duct inlet at and 1.2.

		Mass flow ratio	Total pressure recovery	Exit Mach number	Exit pressure ratio
2	T	0.06	0.48	0.56	2.93
	E	0.32	0.84	1.52	1.68
	S	0.21	0.89	1.60	1.61
1.2	T	0.06	0.76	0.53	1.47
	E	0.25	0.90	0.84	1.38
	S	0.15	0.89	1.16	0.92