Research Article
Parametric Study of Fuel Distribution Effects on a Kerosene-Based Scramjet Combustor
Table 2
Design space for DOE.
| Parameter () | Value |
| ϕ1 | [0.0, 0.15, 0.30, 0.45, 0.6] | ϕ2 | [0.0, 0.15, 0.30, 0.45, 0.6] | ϕ3 | [0.0, 0.15, 0.30, 0.45, 0.6] | ϕ4 | [0.0, 0.15, 0.30, 0.45, 0.6] | |
|
|