Research Article

Landing Gear Aerodynamic Noise Prediction Using Building-Cube Method

Figure 14

Computed mean velocity component at cross section 𝑥 = 0 . 0 (left: BACK_TEAR, center: FRONT_TEAR, right: NO_TEAR).
632387.fig.0014a
(a) Velocity component in the freestream direction
632387.fig.0014b
(b) Velocity component in the vertical direction