Research Article

Landing Gear Aerodynamic Noise Prediction Using Building-Cube Method

Figure 20

Computed mean velocity component at cross section 𝑧 = 2 . 2 1 (left: NO_TEAR, right: NO_SEAL).
632387.fig.0020a
(a) Velocity component in the freestream direction
632387.fig.0020b
(b) Velocity component in the horizontal direction