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] | | |
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