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

Table 2

Mass-averaged performance of the single-duct inlet under both design and off-design conditions.

	Mass flow ratio	Total pressure recovery	Exit Mach number	Exit pressure ratio
6	1	0.61	2.96	20.83
4.5	0.88	0.66	2.09	18.75