Numerical Investigation on the Effect of Fuel-Rich Degree in the RBCC Engine under the Ejector Mode

Table 3

The mass fraction of the rocket plume with different mixing ratios ().

	Mass fraction of C12H23	Mass fraction of CO2	Mass fraction of H2O
1.6	13.73%	61.96%	24.31%
2.0	9.80%	64.78%	25.42%
2.4	6.54%	67.12%	26.34%
2.8	3.77%	69.11%	27.12%
3.2	1.40%	70.81%	27.79%