International Journal of Aerospace Engineering

Research Article

Parametric Study of Fuel Distribution Effects on a Kerosene-Based Scramjet Combustor

Table 3

Fuel injection conditions for Cases  1–4.
 ϕ1ϕ2ϕ3ϕ4
Case  0.450.00.00.0
Case  0.00.450.00.0
Case  0.00.00.450.0
Case  0.00.00.00.45