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

Table 1

Summary of the flight conditions for the different working modes.

Case		Density (kg/m^3)	Pressure (Pa)	Re (×10^6)	Grid (×10^6)
Single duct	6	0.025	1616.17	2.52	3.6
	4.5	0.046	2971.69	3.06
Dual ducts	4	0.064	4047.42	4.24	6.8
	3	0.112	6994.78	5.54
Tri-ducts	2	0.246	15327.56	8.11	8.6
	1.2	0.651	46415.57	13.8