Table 3 Details of input factors in the matrix of experiments
From: A Parametric study on the effects of winglet cant angle on wing aerodynamics and aeroacoustics
Factor | Unit | Label | Range |
|---|---|---|---|
Pressure | [kPa] | A | \([26.5,\,101.3]\) |
Temperature | [K] | B | \([224,\,300]\) |
Mach Number | [-] | C | \([0.3,\,0.8]\) |
Angle of Attack | [\(^\circ\)] | D | \([0,\,20]\) |
Cant Angle | [\(^\circ\)] | E | \([-90,\,150]\) |
