Numerical Investigation of Inlet Thermodynamic Conditions on Solid Fuel Ramjet Performances

Table 2

Simulation conditions.

Case		S	Mach number	(kg/s)	Inlet temperature (K)
A	1	0	2	0.3	540
	2	0.6	2	0.3	540
	3	0.74	2	0.3	540
B	1	0.6	2	0.3	540
	2	0.6	2	0.4	540
	3	0.6	2	0.5	540
C	1	0.6	2	0.3	500
	2	0.6	2	0.3	540
	3	0.6	2	0.3	580