Numerical Investigation of Inlet Thermodynamic Conditions on Solid Fuel Ramjet Performances

Table 4

Thermodynamic parameters for the cases with different inlet conditions.

Case		(N)	(s)	(m/s)	(mm/s)			(kg/s)
A	1	165	1265	983	0.12	23.07	14.8	0.013	1.56
	2	198	1038	1069	0.18	15.73	14.8	0.0191	1.06
	3	211	997	1089	0.20	14.12	14.8	0.0212	0.954
B	1	198	1038	1069	0.18	15.73	14.8	0.0191	1.06
	2	303	1156	1395	0.25	15.27	14.8	0.0262	1.03
	3	406	1246	1712	0.31	15.34	14.8	0.0326	1.04
C	1	193	1076	1055	0.17	16.73	14.8	0.0179	1.13
	2	198	1038	1069	0.18	15.73	14.8	0.0191	1.06
	3	204	1004	1074	0.19	14.77	14.8	0.0203	0.998