Research Article

Landing Gear Aerodynamic Noise Prediction Using Building-Cube Method

Figure 18

Computed mean velocity component in the horizontal direction at cross section 𝑦 = 0 . 2 ( left: BACK_TEAR, right: BACK_SEAL).
632387.fig.0018a
(a) Velocity component in the freestream direction
632387.fig.0018b
(b) Velocity component in the vertical direction