Research Article

Landing Gear Aerodynamic Noise Prediction Using Building-Cube Method

Figure 15

Computed mean velocity component at cross section 𝑦 = 0 . 0 (left: BACK_TEAR, center: FRONT_TEAR, right: NO_TEAR).
632387.fig.0015a
(a) Velocity component in the freestream direction
632387.fig.0015b
(b) Velocity component in the vertical direction