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

Table 3

Mass-averaged performance of the dual-duct inlet at and 3.

		Mass flow ratio	Total pressure recovery	Exit Mach number	Exit pressure ratio
4	E	0.51	0.63	2.60	3.89
	S	0.32	0.76	2.91	3.19
3	E	0.40	0.65	1.97	2.74
	S	0.34	0.84	2.06	3.59