Research Article

Landing Gear Aerodynamic Noise Prediction Using Building-Cube Method

Figure 19

Computed mean velocity component at cross section 𝑧 = 2 . 2 1 ( left: BACK_TEAR, right: BACK_SEAL).
632387.fig.0019a
(a) Velocity component in the freestream direction
632387.fig.0019b
(b) Velocity component in the horizontal direction