A Preliminary Research on Combustion Characteristics of a Novel-Type Scramjet Combustor

Table 1

(a) Geometry parameters of the present model; (b) detailed boundary condition.

(a)

50 mm

300 mm

10 mm

55 mm

45 mm

10 mm

38 mm

10 mm

4 mm

(b)

Inlet	Pressure (MPa)	Temperature (K)	Velocity (m/s)
	1.5	650	762
Fuel nuzzle	Pressure (MPa)	Temperature (K)	Velocity (m/s)
	2	1800	1362
Outlet	Pressure (Pa)	Temperature (K)
	101325	300
Symmetric faces	Symmetric boundary condition
Walls	Nonslip adiabatic boundary condition